From 6eff6a7e0223de57980f3311f3011152158ac5d5 Mon Sep 17 00:00:00 2001 From: hechao <490956681@qq.com> Date: Mon, 19 Jun 2023 11:06:28 +0800 Subject: [PATCH] =?UTF-8?q?=E6=96=B0=E5=A2=9ELBM=E7=AE=97=E4=BE=8B6?= =?UTF-8?q?=E4=B8=AA?= MIME-Version: 1.0 Content-Type: text/plain; charset=UTF-8 Content-Transfer-Encoding: 8bit --- .../30p30n结构重叠网格说明文档.pdf | Bin 456222 -> 0 bytes .../bin/boundary_condition.hypara | 60 - .../bin/cfd_para.hypara | 1220 ----------- .../bin/overset.txt | 17 - .../补充说明.txt | 2 - .../bin/boundary_condition_ref.hypara | 61 - .../bin/cfd_para_incompressible.hypara | 215 -- .../bin/grid_para.hypara | 30 - .../bin/key.hypara | 52 - .../grid/网格地址.txt | 5 - .../bin/boundary_condition_ref.hypara | 73 - .../bin/cfd_para_incompressible.hypara | 214 -- .../bin/grid_para.hypara | 30 - .../grid/网格地址.txt | 5 - .../bin/boundary_condition_ref.hypara | 68 - .../bin/cfd_para_incompressible.hypara | 197 -- .../bin/grid_para.hypara | 30 - .../grid/网格地址.txt | 5 - .../bin/boundary_condition_ref.hypara | 71 - .../bin/cfd_para_incompressible.hypara | 202 -- .../bin/grid_para.hypara | 30 - .../grid/网格地址.txt | 5 - .../bin/boundary_condition_ref.hypara | 63 - .../bin/cfd_para_incompressible.hypara | 212 -- .../bin/grid_para.hypara | 30 - .../grid/网格地址.txt | 5 - .../bin/cfd_para.hypara | 1055 ++++----- L01_TwoD_Cavity_BGK_MPI_1CPU/bin/input.txt | 35 + .../bin/key.hypara | 7 +- .../bin/cfd_para.hypara | 1055 ++++----- .../bin/input.txt | 35 + .../bin/key.hypara | 7 +- .../bin/cfd_para.hypara | 1055 ++++----- .../bin/input.txt | 35 + .../bin/key.hypara | 7 +- .../bin/cfd_para.hypara | 1055 ++++----- L04_ThreeD_Spoiler_BGK_MPI_8CPU/bin/input.txt | 35 + .../bin/key.hypara | 55 + L04_ThreeD_Spoiler_BGK_MPI_8CPU/mesh_3d.dat | 1937 +++++++++++++++++ .../bin/cfd_para.hypara | 1467 +++++++++++++ L05_TwoD_Cavity_BGK_OMP_1CPU/bin/input.txt | 33 + L05_TwoD_Cavity_BGK_OMP_1CPU/bin/key.hypara | 58 + .../bin/cfd_para.hypara | 1467 +++++++++++++ L06_TwoD_Spoiler_BGK_OMP_4CPU/bin/input.txt | 33 + .../bin/key.hypara | 7 +- L06_TwoD_Spoiler_BGK_OMP_4CPU/mesh_2d.dat | 303 +++ 46 files changed, 7765 insertions(+), 4878 deletions(-) delete mode 100644 F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/30p30n结构重叠网格说明文档.pdf delete mode 100644 F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/bin/boundary_condition.hypara delete mode 100644 F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/bin/cfd_para.hypara delete mode 100644 F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/bin/overset.txt delete mode 100644 F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/补充说明.txt delete mode 100644 H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/boundary_condition_ref.hypara delete mode 100644 H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/cfd_para_incompressible.hypara delete mode 100644 H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/grid_para.hypara delete mode 100644 H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/key.hypara delete mode 100644 H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/grid/网格地址.txt delete mode 100644 H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/boundary_condition_ref.hypara delete mode 100644 H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/cfd_para_incompressible.hypara delete mode 100644 H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/grid_para.hypara delete mode 100644 H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/grid/网格地址.txt delete mode 100644 H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/boundary_condition_ref.hypara delete mode 100644 H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/cfd_para_incompressible.hypara delete mode 100644 H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/grid_para.hypara delete mode 100644 H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/grid/网格地址.txt delete mode 100644 H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/boundary_condition_ref.hypara delete mode 100644 H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/cfd_para_incompressible.hypara delete mode 100644 H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/grid_para.hypara delete mode 100644 H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/grid/网格地址.txt delete mode 100644 H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/boundary_condition_ref.hypara delete mode 100644 H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/cfd_para_incompressible.hypara delete mode 100644 H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/grid_para.hypara delete mode 100644 H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/grid/网格地址.txt rename {H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU => L01_TwoD_Cavity_BGK_MPI_1CPU}/bin/cfd_para.hypara (60%) create mode 100644 L01_TwoD_Cavity_BGK_MPI_1CPU/bin/input.txt rename {H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU => L01_TwoD_Cavity_BGK_MPI_1CPU}/bin/key.hypara (91%) rename {H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU => L02_ThreeD_Channel_Turb_BGK_MPI_32CPU}/bin/cfd_para.hypara (60%) create mode 100644 L02_ThreeD_Channel_Turb_BGK_MPI_32CPU/bin/input.txt rename {H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU => L02_ThreeD_Channel_Turb_BGK_MPI_32CPU}/bin/key.hypara (91%) rename {H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU => L03_ThreeD_Poiseuille_MRT_MPI_4CPU}/bin/cfd_para.hypara (60%) create mode 100644 L03_ThreeD_Poiseuille_MRT_MPI_4CPU/bin/input.txt rename {H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU => L03_ThreeD_Poiseuille_MRT_MPI_4CPU}/bin/key.hypara (91%) rename {H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU => L04_ThreeD_Spoiler_BGK_MPI_8CPU}/bin/cfd_para.hypara (60%) create mode 100644 L04_ThreeD_Spoiler_BGK_MPI_8CPU/bin/input.txt create mode 100644 L04_ThreeD_Spoiler_BGK_MPI_8CPU/bin/key.hypara create mode 100644 L04_ThreeD_Spoiler_BGK_MPI_8CPU/mesh_3d.dat create mode 100644 L05_TwoD_Cavity_BGK_OMP_1CPU/bin/cfd_para.hypara create mode 100644 L05_TwoD_Cavity_BGK_OMP_1CPU/bin/input.txt create 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z&+&lgc))X@J{%4Ycn;KuLvg_I3h*4L4~O~!c>tc{0ndT@aOhMSdtL(6heL6|_5eHw z>cgSF!1w?>2kOJ2zQBG3c#fWgfIZd$*XKZeICN-5x-FI24E7uYme+C=QzkP#+G( zVaEqh9}dM~w+B!k4qf^Ic>vevKz%sW7rS2p_2Ez)c6DcER38rW`y+Ic zO|S3spJ&pbHu~q9|I>y5pr02nZKL1IxU`M_JKQC0sASxdXTG4F6!UB%dKUC&c4-@W&h4wJe84QUT5!c z*3RM22U4LbN$AE1=5>4a$f?RRulxO!Dskp@|8Evg?6{q=(~duv>W|05YB*S-AJNUv Qw53aqZpbH4|620@1tVn|vH$=8 diff --git a/F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/bin/boundary_condition.hypara b/F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/bin/boundary_condition.hypara deleted file mode 100644 index b20c191..0000000 --- a/F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/bin/boundary_condition.hypara +++ /dev/null @@ -1,60 +0,0 @@ -# nBoundaryConditons : number of global boundary conditions. -# bcName : Boundary Condition Name. -# bcType(in PHengLEI): Boundary Condition Type. - -# Account of how to set boundaryconditon. -# string bcName = "Farfield"; -# { -# int bcType = 4; -# int inflowParaType = 1; -# double attackd = 0; -# double refReNumber = 6.5e6; -# double refMachNumber = 3.5; -# double angleSlide = 0; -# } - -int nBoundaryConditons = 7; -string bcName = "SOLID_SURFACE"; -{ - int bcType = 2; -} -string bcName = "Wall_16"; -{ - int bcType = 16; -} -string bcName = "Wall_17"; -{ - int bcType = 17; -} -string bcName = "Wall_18"; -{ - int bcType = 18; -} -string bcName = "SYMMETRY"; -{ - int bcType = 3; -} -string bcName = "FARFIELD"; -{ - int bcType = 4; -} -string bcName = "POLE1"; -{ - int bcType = 71; -} - -# 'bcType' is defined as following: -# 99: PERIODIC -# -2: WAKE -# -1: INTERFACE -# 0 : NO_BOUNDARY_CONDITION -# 1 : EXTRAPOLATION -# 2 : SOLID_SURFACE -# 3 : SYMMETRY -# 4 : FARFIELD -# 5 : INFLOW -# 6 : OUTFLOW -# 52: PRESSURE_INLET -# 62: PRESSURE_OUTLET -# 61: OUTFLOW_CONFINED -# 7 : POLE diff --git a/F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/bin/cfd_para.hypara b/F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/bin/cfd_para.hypara deleted file mode 100644 index b17970c..0000000 --- a/F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/bin/cfd_para.hypara +++ /dev/null @@ -1,1220 +0,0 @@ -//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ -// PPPPP H H EEEEE N N GGGGG L EEEEE III + -// P P H H E NN N G L E I + -// PPPPP HHHHH EEEEE N N N G GG L EEEEE I + -// P H H E N N N G G L E I + -// P H H EEEEE N N GGGGG LLLLL EEEEE III + -//------------------------------------------------------------------------+ -// Platform for Hybrid Engineering Simulation of Flows + -// China Aerodynamics Research and Development Center + -// (C) Copyright, Since 2010 + -//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ -########################################################################### -# Default parameters for Grid conversion # -########################################################################### -// gridtype: Grid type for generation, conversion, reconstruction, merging. -// 0 -- Unstructured grid. -// 1 -- Structured grid. -// 2 -- Hybrid grid, include both of unstructured and structured grid. -// gridobj: Task type of grid treatment. -// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc. -// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS. -// 2 -- Grid refinement. -// 3 -- Grid merging, merge two blocks into one block. -// 4 -- Grid deformation, achieve unstructured grid deformation. -// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells. -// 6 -- Grid mirroring, mirror a symmetry grid to whole grid. -// multiblock: Multi-block grid or not, only for structured grid conversion. -// 0 -- Not. -// 1 -- Yes. -// iadapt: Adaptation number for unstructure grid. -// SymmetryFaceVector: The vector of symmetry face. -// 0 -- X axis. -// 1 -- Y axis. -// 2 -- Z axis. -int gridtype = 0; -int gridobj = 1; -int multiblock = 0; -int iadapt = 0; -int SymmetryFaceVector = 1; - -// axisup: Type of Cartisien coordinates system, used in grid conversion. -// 1 -- Y upward. (default) -// 2 -- Z upward. -int axisup = 1; - -// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". -// 0 -- Interface. (default) -// 1 -- Physical boundary condition, used in Hybrid solver. -int omit_no_bound_bc = 0; - -//----------------------------------------------------------------------- -# Grid data type # -//----------------------------------------------------------------------- -// from_gtype/to_gtype: Type of grid data type in grid conversion process. -// -1 -- MULTI_TYPE. -// 1 -- PHengLEI, *.fts. -// 2 -- CGNS, *.cgns. -// 3 -- Plot3D type of structured grid, *.dat/*.grd. -// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. -// 5 -- Fluent, *.cas/*.msh. -// 6 -- Ustar, mgrid.in. -// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. -// 8 -- GMSH, *.msh. -// dumpOldGrid: If dump out the old grid file. -// 0 -- Not. (default) -// 1 -- Yes. -int from_gtype = 2; -int to_gtype = 1; -int dumpOldGrid = 0; - -//----------------------------------------------------------------------- -# File path # -//----------------------------------------------------------------------- -// from_gfile: path of original data file for unstructure grid convert from. -// out_gfile: path of target file for grid convert to, *.fts type of file usually. -int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; - -// ----------------- some advanced choices ------------------------------ -// iunsteady: The Grid is for unsteady simulation or not. -int iunsteady = 0; -int codeOfAleModel = 0; - -// fileformat: Ustar Grid file format. -// 0 -- BINARY. -// 1 -- ASCII. -int fileformat = 0; - -// Parameters for hybrid solver. -// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type. -// mixgrid_str: path of structure grid file for hybrid solver, *.fts type. -string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; -string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; - -// Some parameters for structured overlapping grid. -int codeOfDigHoles = 1; -string holeBasicFileName = "./oversetGridView/holeBasicFile.inp"; -string holeFullFileName = "./oversetGridView/holeFullFile.dat"; -string linkFileName = "./oversetGridView/topology.dat"; -string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; - -// ----------------- Adaptive Mesh Refine ------------------------------- -// In this file, the original_grid_file is used of the partition part. -// If use it dependently, abstract it here. -string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts"; -string geometryFileName = "./grid/jsm.igs"; - -// geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. -// exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. -// projectOrgPoint: If the original wall points need to be projected or not. -int geometryUnit = 1; -int anisoRefine = 0; -int isProject = 0; -int readDist = 0; -int isDeform = 0; -int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT. -int projectOrgPoint = 0; // if project original wall points. - - -// ----------------- Grid Deform Parameters ----------------------------- -// deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. -// stationalGridFile: Original grid file. -// visualFileName : The visualization file path of deform grid. -// nDeformStep : The max deform step. -// flapAngle : The max flap angle. -// rotatePostionZ : Rotate postion. -// rotatePostionY : Rotate postion. -// gridSlice : If dump slice grid. -// sliceAxis : Grid slice axis. -// slicePosition : Grid slice position. -int nDeformStep = 40; -double flapAngle = 10.0; -double rotatePostionZ = 4.00003; -double rotatePostionY = 3.05; - -int deformationMethod = 2; -string stationalGridFile = "./grid/Segment2Brid.fts"; -string visualFileName = "./results/deformedGrid.dat" - -int gridSlice = 1; -int sliceAxis = 1; -double slicePosition = 13; - -// ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. -int numberOfReferenceCP = 40; -double influencePara = 25.0; - -// ----------------- Periodic Parameters -------------------------------- -// Notice: Rotational periodicity only support rotation along the X axis! -// periodicType: Which periodic boundary is used. -// 0 -- without Periodic Boundary. -// 1 -- Translational periodicity. -// 2 -- Rotational periodicity. -// translationLength[]: The relative distance between two periodic face - which only support one direction. -// rotationAngle: The relative angle between two periodic face. - which is recorded in degrees. - -int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; -double rotationAngle = 0.0; - -######################################################################### -# Default parameters for Partition # -######################################################################### -// pgridtype: The grid type. -// 0 -- unstruct grid. -// 1 -- struct grid. -// 2 -- refine structured grid. -// maxproc: The number of partition zones that want to be divided into. -int pgridtype = 0; -int maxproc = 4; - -// traceMark: Trace mark or not, only for structured grid partition. -// 0 -- Not. -// 1 -- Yes. -// blockIndexOfMark: the block index of mark, only for structured grid partition. -// cellIndexOfMark: the cell index of mark, only for structured grid partition. -int traceMark = 0; -int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; - -// parallel Strategy: -//! -# 0 : each zone is assigned to the one that defined in grid partition procedure. -//! -# 1 : random assigned for each zone or by some else ways. -int parallelStrategy = 1; - -//----------------------------------------------------------------------- -# File path # -//----------------------------------------------------------------------- -// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). -// partition_grid_file: Target partition grid file(PHengLEI type, *.fts). -string original_grid_file = "./grid/sphere_mixed.fts"; -string partition_grid_file = "./grid/sphere_mixed__4.fts"; - -// ------------------ Sompe advanced parameters ------------------------- -// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". -// 0 -- Interface. (default) -// 1 -- Physical boundary condition, used in Hybrid solver. -// npartmethod: Method of interface reconstruction, default is 1. -// parallelPartitionMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition. -// 1 -- Using ParMetis for homogeneous MPI. -// 2 -- Using Metis for homogeneous MPI. -// 3 -- using METIS partition for homogeneous OpenMP. -// parmetisBalance: Used to specify the imbalance tolerance. -// 1 -- perfect balance. -// maxproc -- perfect imbalance. -// 1.05 -- recommended. - -int omit_no_bound_bc = 0; -int npartmethod = 1; -int parallelPartitionMethod = 2; -double parmetisBalance = 1.05; - -// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. -// 1 -- single level. -// 2 -- 2 level. -// N -- N level, ..., et al. -int numberOfMultigrid = 1; - -######################################################################### -# Default parameters for CFD simulation # -######################################################################### -// maxSimuStep: The max simulation step, don't care simulation is restart or not. -// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. -// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. -// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved. -// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. -// intervalStepRes: The step intervals for residual file 'res.dat' saved. -// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. -// 0 -- no precondition process. (default, mach > 0.3) -// 1 -- carry out precondition process. (mach number <= 0.3) - -int maxSimuStep = 20000; - -int intervalStepFlow = 1000; -int intervalStepPlot = 1000; -int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; - -// compressible: -// 0 -- incompressible flow. -// 1 -- compressible flow. (default) -int compressible = 1; - -//----------------------------------------------------------------------- -# CFD Control Parameter # -//----------------------------------------------------------------------- -// refMachNumber: Mach number. -// attackd: Angle of attack. -// angleSlide: Angle of sideslip. -// inflowParaType: The type of inflow parameters. -// 0 -- the nondimensional conditions. -// 1 -- the flight conditions. -// 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. -// 4 -- the condition that the velocity, temperature and density are given. -// 5 -- the condition that the velocity, temperature and pressure are given. -// refReNumber: Reynolds number, which is based unit length, unit of 1/m. -// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. -// freestream_vibration_temperature: Dimensional freestream vibration temperature. -// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition. -// height: Fly height, unit of km. -// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition. -// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like: -// 1 dm = 0.1 m. -// 1 cm = 0.01 m. -// 1 mm = 0.001m. -// 1 inch = 0.0254m. -// 1 foot = 12 inches = 0.3048m. -// 1 yard = 3 feet = 0.9144m. -// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit. -// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit. -// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary -// condition is radiation equilibrium temperature, and 0.8 is the default value. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. -// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on. - -double refMachNumber = 0.73; -double attackd = 2.79; -double angleSlide = 0.00; - -int inflowParaType = 0; -double refReNumber = 6.5e6; -double refDimensionalTemperature = 288.15; -double freestream_vibration_temperature = 300.00; - -//int inflowParaType = 1; -//double height = 0.001; - -//int inflowParaType = 2; -//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2). -//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)). - -//int inflowParaType = 3; -//int nsubsonicInlet = 1; -//int nsubsonicOutlet = 1; -//string inLetFileName = "./bin/subsonicInlet.hypara"; -//string outLetFileName = "./bin/subsonicOutlet.hypara"; -//double refDimensionalTemperature = 288.144; -//double refDimensionalPressure = 1.01313E05; - -//The velocity, temperature and density are fixed. -//int inflowParaType = 4; -//double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; - -//The velocity, temperature and pressure are fixed. -//int inflowParaType = 5; -//double refDimensionalVelocity = 1000.0; -//double refDimensionalPressure = 1.0e5; - -//The MachNumber, temperature and pressure are fixed. -//int inflowParaType = 6; -//double refDimensionalTemperature = 293; -//double refDimensionalPressure = 8886.06; - -double wallTemperature = -1.0; - -double radiationCoef = 0.8; -double gridScaleFactor = 1.0; - -int numberOfAerodynamicForceComponents = 1; -double forceReferenceLengthSpanWise = 1.0; // unit of meter. -double forceReferenceLength = 1.0; // unit of meter. -double forceReferenceArea = 1.0; // unit of meter^2. -double TorqueRefX = 0.0; // unit of meter. -double TorqueRefY = 0.0; // unit of meter. -double TorqueRefZ = 0.0; // unit of meter. -double refMolecularWeight = 28.9644; // unit of g/mol. - -//----------------------------------------------------------------------- -# Spatial Discretisation # -//----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* -// inviscidSchemeName: Spatial discretisation scheme of struct grid. -// Using this when solve structered grid or hybrid. -// -- "vanleer", "steger", "hlle", "lax_f". -// -- "roe", "modified_roe". -// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+". -// str_limiter_name: Limiter of struct grid. -// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth". -// -- "nolim", no limiter. -// -- "vanalbada_clz", clz supersonic version. -string inviscidSchemeName = "roe"; -string str_limiter_name = "vanalbada"; - -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* -// viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. -// viscousName: Laminar or tubulent model. -// -- "0eq-bl". -// -- "1eq-sa". -// -- "2eq-kw-menter-sst". -// -- "2eq-kw-menter-bsl". -// -- "2eq-kw-wilcox-1988". -// -- "2eq-kw-wilcox-1998". -// -- "2eq-kw-kok-tnt". -// -- "2eq-kw-wilcox-2006". -// -- "easm-kw-2003". -// -- "easm-kw-2005". -// DESType: Type of DES. -// 0 -- RANS. (default) -// 1 -- DES. -// 2 -- DDES. -// 3 -- IDDES. -// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. -// Using this when solve Unstructered grid or hybrid. -// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle". -// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". -// uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". -// -- "nolim", no limiter. -// uns_vis_name: Discretisation method of viscous term. -// -- "std", "test", "aver", "new1", "new2". -// gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". -// ivencat: Variation of vencat limiter. -// 0 -- org method, it is independent of grid scale. -// 1 -- new method, it is dependent of grid scale. -// 4 -- Ustar limiter model, without grid size unitary. -// 7 -- default used. -// venkatCoeff: Cofficient of vencat, when using vencat limter. -// limitVariables: Limit model (It is useful only if limitVector is 0). -// 0 -- limit only for pressure and denstiny, then get the min value. -// 1 -- limit for every variables, then get the min value. -// limitVector: -// 0 -- Each variable use the same limiter coefficient. -// 1 -- Each variable use the respective limiter coefficients. -// reconmeth: -// 0 -- When reconstruct face value, Q+, Q- use respective limiter coefficients. -// 1 -- Q+, Q- use the min limiter coefficients of left and right cell. -// skewnessAngle: The skewness angle of grid cells. -// roeEntropyFixMethod: Entropy fix (correction) method. -// 1 -- direct fix, which limits the minimum eigenvalue directly. -// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver. -// 3 -- Harten type, which is default used. -// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0. -// It is used to scale the default Roe entropy fix coefficients. - -//int viscousType = 0; -//string viscousName = "Euler"; - -//int viscousType = 1; -//string viscousName = "laminar"; - -int viscousType = 3; -string viscousName = "1eq-sa"; - -//int viscousType = 4; -//string viscousName = "2eq-kw-menter-sst"; - -int DESType = 0; - -string uns_scheme_name = "roe"; -string uns_limiter_name = "vencat"; -string uns_vis_name = "test"; -string gradientName = "ggnode"; - -int ivencat = 7; -double venkatCoeff = 5.0; -int reconmeth = 1; -int limitVariables = 0; -int limitVector = 0; -double skewnessAngle = 60.0; - -int roeEntropyFixMethod = 3; -double roeEntropyScale = 1.0; - -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- -// iunsteady: Steady or unsteady. -// 0 -- steady. -// 1 -- unsteay. -// physicalTimeStep: The nondimensional physical time step. -// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes. -// ifStaticsFlowField: Statistical variables for unsteady simulation. -// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation. -// startStatisticStep: Outer step when start statistics. -// when the value is larger than "maxSimuStep", it is useless. -// statisticalTimePeriod: Used as time period of statistic analysis. -// when the value is negative, time period is treated as infinite. -// statisticMethod: Statistic reynolds stress method. - 0 --tau = - ^2 - 1 --tau = -// min_sub_iter: The min sub iteration of unsteady simulation. -// max_sub_iter: The max sub iteration of unsteady simulation. -// tol_sub_iter: The tolerance of sub iteration of unsteady simulation. -// tscheme: Temporal Discretisation method. -// 1 -- Runge-Kutta Multi-State. -// 2 -- Point implicit. -// 3 -- Full implicit. -// 4 -- LU-SGS. -// 5 -- Block LU-SGS. -// 6 -- Jacobian iteration. -// 7 -- Lower G-S iteration. -// 8 -- Upper G-S iteration. -// 9 -- Lower/Upper G-S iteration. -// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. -// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. -// CFLStart: Started cfl number. -// CFLEnd: End cfl number. -// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. -// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) -// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. -// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. -// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS. -// ifLocalTimeStep: Time step method. -// 0 --Local. -// 1 --Global. -// visl_min: Minimum value of laminar viscosity coefficient. -// turbCFLScale: Turbulence model cfl number factor. -// codeOfAleModel: Arbitrary Lagrangian-Eulerian method. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. -// wallFunctionType: The type of wall function to implement. -// 0 -- no wall function. (default) -// 1 -- standard wall function. -// 2 -- Pab3D wall function. -// RKStage: The number of Runge-Kutta step. -// lamda: Cofficient of Runge-Kutta step. - -int iunsteady = 0; -double physicalTimeStep = 0.01; -int ifStartFromSteadyResults = 0; -int ifStaticsFlowField = 0; -int ifStaticsReynoldsStress = 0; -int startStatisticStep = 800000; -double statisticalTimePeriod = -1.0; -int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; - -int methodOfDualTime = 3; -int min_sub_iter = 50; -int max_sub_iter = 50; -double tol_sub_iter = 0.01; - -int tscheme = 4; -int iSimplifyViscousTerm = 1; -int ifLocalTimeStep = 0; -double CFLStart = 0.01; -double CFLEnd = 10.0; -int CFLVaryStep = 500; - -double ktmax = 1.0e10; - -int swapDq = 1; - -int nLUSGSSweeps = 1; -double LUSGSTolerance = 0.01; -int order = 2; - -double visl_min = 0.01; -double turbCFLScale = 1.0; -double csrv = 2.0; -double timemax = 1.0e10; -double dtsave = -1.0; -int maxale = 10; -double dtau = 0.001; - -int wallFunctionType = 0; - -int RKStage = 2; -double lamda[] = 0.5, 1.0; - -//int RKStage = 1; -//double lamda[] = 1.0; - -//int RKStage = 4; -//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- -// numberOfGridGroups: The number of grid groups. -// gridfile: The partitioned Grid file path, using relative path, -// which is relative to the working directory. -// IMPORTANT WARNING: The file index should be ignored, -// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts, -// please use 'rae2822_hybrid2d__4.fts' here! -// plotFieldType: If dump out the field results to visulization. -// walldistMethod: The method to compute wall distance. -// 0 -- accurate but not fast enough. -// 1 -- fast but not accurate enough. -// 2 -- super fast but more non-accurate! -// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps. -// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps. -// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps. -// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps. -// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps. -// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps. -// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps. -// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. -// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. - -int numberOfGridGroups = 1; -string gridfile = "./grid/rae2822_hybrid2d__4.fts"; -string wallTemperaturefile= ""; - -int walldistMethod = 1; - -string resSaveFile = "results/res.dat"; -string turbresfile = "results/turbres.dat"; -string aircoeffile = "results/aircoef.dat"; - -string restartNSFile = "results/flow.dat"; -string turbfile = "results/turb.dat"; - -string visualfile = "results/tecflow.plt"; -string wall_aircoefile = "results/wall_aircoef.dat"; -string samplefile = "results/sample.dat"; - -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; - -string jetDefineFile = "bin/jet.hypara"; - -string sixDofFileName = "results/sixDofInfo.dat"; -string derivativeFileName = "results/identify.dat"; -string hysteresisFileName = "results/force_beta.plt"; - -int plotFieldType = 0; - -// visualfileType: The file type of visualfile. -// 0 -- Tecplot binary. -// 1 -- Tecplot ASCII. - -int visualfileType = 1; - -// samplefileMode: The dump mode of sample file. -// 0 -- dump out every probe/line/surface data for all step intervals. -// 1 -- dump out all probe/line/surface data for every step intervals. -int samplefileMode = 0; - -// visualSlice: The slice of tecflow. -// 0 -- Do not save slice data. -// 1 -- comput and save it to sliceFile. -// sliceAxis: Normal vector of slice. -// 1 -- X_DIR. -// 2 -- Y_DIR. -// 3 -- Z_DIR. -// slicePostion: Coordinate of slice. - -int visualSlice = 0; -int sliceAxis = 1; -double slicePostion = -0.5; -string sliceFile = "results/Slice.plt"; -int dumpWallFaceCenter = 0; - -// min-max box of the visual block. -double lowerPlotFieldBox[] = [0.0 0.0 0.0]; -double upperPlotFieldBox[] = [1.0 1.0 1.0]; - -//-----------the optional parameters list for the flow field output---------------- -// nVisualVariables: Number of variables want to be dumped for tecplot visualization. -// visualVariables : Variable types dumped, listed as following: -// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), -// -- viscosityLaminar(7), viscosityTurbulent(8), -// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12), -// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17), -// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), -// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), -// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), -// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81). -// -- specific heat ratio(gama, 56) -// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! -// Variables order must from small to big. -//-----------the optional parameters list for the wall boundary condition---------------- -// nVisualWallVariables: The number of visual variables on wall. -// visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11), -// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15) -// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19) -// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48), -// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52), -// -overlap iblank(iblank, 81) - -int nVisualVariables = 8; -int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; - -int nVisualWallVariables = 9; -int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; - -// dumpStandardModel: Dump many standard model data. -// 1 -- Turbulent flat plate. -int dumpStandardModel = 0; - -// ifSetDataMonitor: Whether to set the data monitor. -// 0 -- No. -// 1 -- Yes. -// dataMonitorType: The type of data Monitor. -// 0 -- Probes data monitor. -// 1 -- Lines data monitor. -// 2 -- Surfaces data monitor. -// probesDefineFile: Probes location information file. -// nLines: The number of lines need to be monitored. -// linesDefineFile: Lines location information file. -// nSurfaces: The number of surfaces need to be monitored. -// surfacesDefineFile: Surfaces location information file. -// searchCellsMethod: method to search the cell of each probe. -// 0 -- Nearest cell to the probe. -// 1 -- Real cell where the probe is located. -// nProbeVariables: Number of variables want to be dumped for probes monitered. -// probeVariables : Variable types dumped, listed as following: -// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5). -// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!! -// probeVariables order must from small to big. -// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables. -// 0 -- Take the value of probe's cell as probe real value. -// 1 -- Interpolation from probe's and neighbouring cell to probe. -// 2 -- Interpolation from probe's cell nodes to probe. -int ifSetDataMonitor = 0; - -int dataMonitorType = 0; -string probesDefineFile = "bin/probes_XYZ.dat"; - -//int dataMonitorType = 1; -//int nLines = 1; -//string linesDefineFile = "bin/lines_XYZ.dat"; - -//int dataMonitorType = 2; -//int nSurfaces = 4; -//string surfacesDefineFile = "bin/surfaces_XYZ.dat"; - -int searchCellsMethod = 0; - -int nProbeVariables = 6; -int probeVariables[] = [0, 1, 2, 3, 4, 5]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- -// turbInterval: Iteration number of turbulence. -// kindOfTurbSource: Kinds of turbulent source. -// 0 -- Original. -// 1 -- Edwards. -// 2 -- new. -// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. - -int turbInterval = 1; -int turbOrderStruct = 2; -int kindOfTurbSource = 0; -int mod_turb_res = 0; -double turb_relax = 1.0; -double freeStreamViscosity = 1.0e-3; -double muoo = 3.0; -double kwoo = 5.0; -int transitionType = 0; -double turbIntensity = -1.0; -int freeturbIntensitySRModify = 0; -double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int transitionMaFix = 1; - -# maximum eddy viscosity (myt/my) max. -double eddyViscosityLimit = 1.0e10; -int monitor_vistmax = 0; - -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- -// iLES: Create LESSolver or not. -// == 1 - Create LESSolver; -// != 1 - not. -// amplitudeofDisturb: Amplitude of adding disturb. -// disturbstep: Unsteady time step or steady iteration of adding random disturb. -// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. -// = 0 - in only first sub-iter; -// != 0 - in every sub-iter. -// ipraddisturb: Add density and pressure disturb or not. -// ibodyforce: Add body force in source flux of NS equations or not. -// = 0 - not; -// != 0 - Add body force. -// bodyforce: Body force in source flux of NS equations or not. -// utau: friction velocity, using in DNSDisturb. -// sgsmodel: subgrid scale model. -// = "smagorinsky"; -// = "dsmCom"; -// = "wale"; -// = "sigma". -// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak); -// = 2 - pow(deltai * deltaj *deltak, 1/3); -// = 3 - Devloped by Scotti. -// wallDampingFunctionType: = 0 - no wall function; -// = 1 - van Driest; -// = 2 - developed by Dr. Deng Xiaobing; -// = 3 - developed by Piomelli. -// turbViscousCutType: turbulent viscosity cut type. -// = 0 - mu_total = mut + mul; -// = 1 - mu_total = max(mut-mul,0)+ mul; -// = 2 - mu_total = max(mut ,0)+ mul. -// smagConstant: constant of smagorinsky model. -// waleConstant: constant of wale model. -// filterDirection[3]: filter variables in i, j, k direction or not. -// averageDirection[3]: average variables in i, j, k direction or not. -// isotropicConstant: constant of isotropic part of SGS stress. - -int iLES = 0; -string sgsmodel = "smagorinsky"; -int deltaFunctionType = 2; -int wallDampingFunctionType = 1; -int turbViscousCutType = 2; -double smagConstant = 0.1; -double isotropicConstant = 0.0; -double waleConstant = 0.6; -double sigmaConstant = 1.35; -int filterDirection[] = [1, 1, 0]; -int averageDirection[] = [0, 0, 0]; -double testFilterScale = 2.0; -int averageWidth = 1; -int monitorNegativeConstant = 0; - -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- -// dg_high_order: -// 0 -- generic order accuracy. -// 1 -- high order accuracy. -// iapplication: -// 0 -- gas model is fixed in the codes. -// 1 -- gas model is imported from library files. -// iCodeBranch: -// 0 -- The old code version is used for Navier-Stokes. -// 1 -- A new code version is active for Navier-Stokes solver. -// nm: Equation number of the physics, but is out of commision now. -// 4 -- for 2D. -// 5 -- for 3D. -// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas. -// Otherwise, the pure gas with one component is used for perfect gas. -// 0 -- Earth gas. -// 1 -- Mars gas. -// 2 -- Argon. -// 3 -- Nitrogen. -// nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . -// 1 -- used. -// nDensityModify: The type of densitymodify. - -// 0 -- not used. -// 1 -- used. -// nchem: -// 0 -- without chemical reaction flow. -// 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. -// 0 -- perfect gas. -// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). -// nchemsrc: -// 0 -- the source terms are not computed. -// 1 -- the source terms are computed. -// nchemrad: -// 0 -- compute the spectrum radius without considering chemical reaction flow. -// 1 -- compute the spectrum radius that need to count the contribution from chemical reaction flow. -// ntmodel: The thermodynamic temperature model. -// 1 -- One-temperature model. -// 2 -- Two-temperature model. -// 3 -- Three-temperature model. -// nTEnergyModel: the method to computing temperature energy model. -// 0 -- the energy term is computed using the conventional method. -// 1 -- the energy term is computed using the curve fitting method. -// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model. -// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value. -// catalyticCoef: -// 0.0 -- full non-catalytic wall boundary condition. -// 1.0 -- full catalytic wall boundary condition. -// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// nTemperatureJump : the method to calculate the temperature jump. -// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode. -// 1 -- the general method where the iteration is calculated with the translation-rotation temperature. -// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0]. -// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0]. -// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0]. -// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0]. -// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0]. -// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0]. -// staticPressureRelaxCorf: The value is in range of [0.1, 1.0]. -// nIsChemicalFreeze : the flag to freeze the chemical reactions. -// 0 -- not freeze, the chemical reaction sources will be calculated. -// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te -// nDebug: cout the Wrong place and abort -// 0 -- not used. -// 1 -- used. -// nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid -// 0 -- not used. -// 1 -- used. -// nChemcalSourceModified: Modified on ChemcalSource -// 0 -- not used. -// 1 -- used. -// nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. -// isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. -// nViscosityModel: - -// 0 -- Blottner fitting method. -// 1 -- Gupta fitting method. -// nSutherland: -// 0 -- stands for selecting the Blotter curve fits mode. -// 1 -- stands for Sutherland relation. -// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11". -// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. -// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. -// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. -// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing two species without reacting. -// For self-definition model, the gasfile is used to indicate the file path of the new gas model. -// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. -// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. -// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes. - -int dg_high_order = 0; -int iapplication = 0; -int iCodeBranch = 0; -int nm = 5; -int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; - -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; - -int nGasModel = 0; -int nchem = 0; -int nchemsrc = 1; -int nchemrad = 1; -int ntmodel = 1; - -int nEnergyRecycle = 0; -int nSlipBCModel = 0; -int nDensityModify = 1; -int nTEnergyModel = 0; -int nMeanFreePathType = 0; -int nIsChemicalFreeze = 0; -int nIsSuperCatalytic = 1; -int nTemperatureJump = 0; - -double parkVDPower = 0.6; -double catalyticCoef = 0.0; -double sigmaVelocity = 1.0; -double sigmaTemperature = 1.0; -double sigmaMassFraction = 1.0; -double velocitySlipCorrectConstant = 1.0; - -double chemicalRelaxCorf = 1.0; -double chemicalSpectrumRadiusCoef = 1.0; -double viscousSpectrumRadiusCoef = 1.0; -double inviscidSpectrumRadiusCoef = 1.0; -double staticPressureRelaxCorf = 1.0; - -double veTemperatureMin = 30.0; -int nDebug = 0; -int nSpeciesLimit = 0; -int nTurblenceForChemical = 0; -int nViscosityFluxSublevelModified = 0 ; -int nChemcalSourceModified = 0; - -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; -string speciesName = "O, O2, NO, N, N2"; -string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; - -//string speciesName = "O, O2, NO, N, NO+, N2, e-"; -//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0"; - -//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-"; -//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0"; - -//string gasfile = "Mars-Pa8"; -//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; -//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; - -//string gasfile = "DK7"; -//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-"; -//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0"; - -//string gasfile = "Combustion-12"; -//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; -//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; - -//string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; -//string initMassFraction = "1.0, 0.0"; -int nSutherland = 0; -double gamaSpeciesA = 1.4; -double gamaSpeciesB = 1.3; -double molecularWeightSpeciesA = 29.0; -double molecularWeightSpeciesB = 30.0; - -int nChemicalFlowStep = 0; -int ifStartFromPerfectGasResults = 0; - -######################################################################### -// Multi-Grid parameters. -// nMGLevel: The number of level of Multi-Grid. -// <= 1 -- Single-level. -// > 1 -- multi-level. -// MGPreIteration: For each grid, the number of pre-smoothing steps. -// n_post: For each grid, the number of post-smoothing steps. -// MGCoarsestIteration: For the coarest grid the number of smoothing steps. -// MGFasType: V-multi cycle or W-multi cycle. -// 1 -- V-multi cycle. -// 2 -- W-multi cycle. -// flowInitStep: Flow initialization step, 0 - 500 is suggested. -// Multi-Grid : Number of steps computing on coarse grid, during flow initialization. -// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization. -// mgCFLScale: CFL number enlarge times for coarse grid. -// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid. -// 1 -- zero order. -// 2 -- first-order. (default) -// mgCorrectionLimit: Multi-grid correction limit. - -int nMGLevel = 1; -int MGCoarsestIteration = 1; -int MGPreIteration = 1; -int MGFasType = 1; -int n_post = 0; -int flowInitStep = 100; -int mprol = 2; -double mgCFLScale = 1.0; -double mgCorrectionLimit = 0.01; - -//--------------- Some parameter for turbulent model -------------------- -// neasm: The variation of kw turbulent model. -// ismooth_turb: Residual smooth for turb or not. -// SSTProductType: The type of product term based on vorticity for SST. -// SAProductType: The type of product term based on vorticity for SA. -int neasm = -3; -int SSTProductType = 0; -int ismooth_turb = 0; -int SAProductType = 2; - -// ----------------- Overset Grid parameter ----------------------------- -int codeOfDigHoles = 1; -int codeOfTurbulentModel = 0; -string masterFileName = "./grid/searchFile.inp"; -string holeBasicFileName = "./grid/holeBasicFile.inp"; -string holeFullFileName = "./grid/holeFullFile.dat"; -string linkFileName = "./grid/topology.dat"; -string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; - -######################################################################### -# High Order Struct Solver # -######################################################################### -// isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. -// SolverStructOrder: Spatial discretisation order of NS equations with struct grid. -// <= 2 -- finite volume method. -// >= 3 -- finite difference order. (to be completed) -// 0 -- default. -// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence, -// smaller epsilon, robuster for shock-detecting. -// str_highorder_interpolation_type: -// -- "classical", "test". -// str_highorder_flux_name: -// -- "roe", "steger". -// structhighordergradient: -// -- "conservation", "chain_rule". -int isFVMOrFDM = 0; -string str_highorder_solver = "WCNS"; -int SolverStructOrder = 0; -double str_highorder_interpolation_epsilon = 1.0e-6; -string str_highorder_interpolation_type = "test"; -string str_highorder_flux_name = "steger"; -string structhighordergradient = "conservation"; -double coefofstrflux = 0.5; -double limitcoefofinterface = 0.0; - -// ----------------- Advanced choices ----------------------------------- -// outtimesc: Time stepping scheme for the outer loop. -// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1]. -// -1 -- seconde-order fully-upwind differencing. -// 0 -- seconde-order upwind-biased differencing. -// 0.333333 -- third-order upwind-biased differencing. -// 1 -- seconde-order central differencing. -// MUSCLCoefXb: The limiter parameter. -// 0 -- the effect of the limiter is cancelled, means the first-order interpolations. -// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1. -string outtimesc = "impbd2"; -double MUSCLCoefXk = -1; -double MUSCLCoefXb = 1.0; -int allReduceStep = 1; - -// ----------------- overlap configuration ------------------------------ -// codeOfOversetGrid: Overlapping(overset) grid or not. -// 0 -- NON-overlapping grid. -// 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation -// 0 -- set the acceptor cell value by donor cell value. -// 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 1; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.ovs"; -double walldistMainZone = 1.0 -double toleranceForOversetSearch = 1.0e-3; -double toleranceForOversetBox = 1.0e-3; -int twoOrderInterpolationOrNot = 0; -int keyEnlargeOfActiveNodes = 0; -int outTecplotOverset = 0; - -int numberOfMovingBodies = 2; - -// ----------------- ALE configuration ------------------------------ -int codeOfAleModel = 1; -int aleStartStrategy = -1; - -int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd; -int strategyForGCLSource = 0; //0-present; 1-Ahn; - -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton -int methodForKineticEquation = 0; -double relaxParameterOfKinetic = 1.0; - -######################################################################### -# motive information # -######################################################################### -int numberOfMovingBodies = 1; - -############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. -// -1 given motion partten. -// 0 still. -// 1 six DOF motion. -// 2 three DOF motion. -// 11 X-axis forced motion. -// 12 Y-axis forced motion. -// 13 Z-axis forced motion. -// 14 forced pitch motion. -// 15 forced yaw motion. -// 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; -//additional force (system axis) fX fY fZ -double addedForce_0[] = 0.0 ,0.0 ,0.0 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; - - -// ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; -//@double refReNumber = 6.5e6; -//@double refDimensionalTemperature = 288.15; -//@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; -//@double refDimensionalVelocity = 0; -//@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### -int isPlotVolumeField = 0; - diff --git a/F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/bin/overset.txt b/F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/bin/overset.txt deleted file mode 100644 index 33cf929..0000000 --- a/F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/bin/overset.txt +++ /dev/null @@ -1,17 +0,0 @@ -int taskSelector = 1; - -int codeOfLargeScale = 0; -int numberOfMultigrid = 1; -int numberOfProcessors = 4; - -string originalGridFile = "./grid/30p30n_str_3D.grd"; -string originalBoundaryFile = "./grid/30p30n_str_3D.inp"; - -int numberOfGridGroups = 4; -int zoneSpan[numberOfGridGroups] = 3,4,4,5; - -int solidBcSize = 2; -int solidColorList[solidBcSize] = 2,4; - -int outerBcSize = 3; -int outerColorList[outerBcSize] = 16,17,18; diff --git a/F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/补充说明.txt b/F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/补充说明.txt deleted file mode 100644 index 24b3bee..0000000 --- a/F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU/补充说明.txt +++ /dev/null @@ -1,2 +0,0 @@ -针对本算例，风雷代码cmake构建的时候需要勾选USE_OVERSET选项！！！ -该算例当前只支持2171版本 \ No newline at end of file diff --git a/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/boundary_condition_ref.hypara b/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/boundary_condition_ref.hypara deleted file mode 100644 index 7ab6817..0000000 --- a/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/boundary_condition_ref.hypara +++ /dev/null @@ -1,61 +0,0 @@ -# nBoundaryConditions: Number of global boundary conditions. -# bcName : Boundary condition name. -# bcType(in PHengLEI): Boundary condition type. - -# How to set boundary condition, for example: -# string bcName = "Wall"; -# { -# int bcType = 2; -# int viscousType = 1; -# double wallTemperature = -1.0; -# double uWall = 0.0; -# double vWall = 0.0; -# double wWall = 0.0; -# } -# string bcName = "Inflow"; -# { -# int bcType = 5; -# int inflowParaType = 0; -# double refMachNumber = 0.73; -# double attackd = 2.79; -# double angleSlide = 0.0; -# double refReNumber = 6.5e6; -# double refDimensionalTemperature = 288.15; -# } - -# For more information, see examples/bin/boundary_condition.hypara file!!! - -int nBoundaryConditions = 3; -string bcName = "wall"; -{ - string bodyName = "body"; - int bcType = 2; - string flowType = "FLOW_SOLID_SURFACE"; -} -string bcName = "inlet"; -{ - int bcType = 5; - string flowType = "FLOW_VELOCITY_INLET"; - double flowU =0.9191874; -} -string bcName = "outlet"; -{ - int bcType = 6; - string flowType = "FLOW_PRESSURE_OUTLET"; - double flowP =0; -} - -# 'bcType' is defined as following: -# -2: WAKE -# -1: INTERFACE -# 0 : NO_BOUNDARY_CONDITION -# 1 : EXTRAPOLATION -# 2 : SOLID_SURFACE -# 3 : SYMMETRY -# 4 : FARFIELD -# 5 : INFLOW -# 6 : OUTFLOW -# 52: PRESSURE_INLET -# 62: PRESSURE_OUTLET -# 61: OUTFLOW_CONFINED -# 7 : POLE diff --git a/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/cfd_para_incompressible.hypara b/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/cfd_para_incompressible.hypara deleted file mode 100644 index a2026d7..0000000 --- a/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/cfd_para_incompressible.hypara +++ /dev/null @@ -1,215 +0,0 @@ -######################################################################### -# General Control Parameter # -######################################################################### -// nIsComputeWallDist: Whether to compute the wall distance. -// 0 -- Compute wall distance. -// 1 -- Not compute. -// gridfile: The partitioned Grid file path, using relative path, -// which is relative to the working directory. -// maxSimuStep: The max simulation step, don't care simulation is restart or not. -// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. -// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. -// intervalStepRes: The step intervals for residual 'res.dat' saved. -// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like: -// 1 dm = 0.1 m. -// 1 cm = 0.01 m. -// 1 mm = 0.001m. -// 1 inch = 0.0254m. -// 1 foot = 12 inches = 0.3048m. -// 1 yard = 3 feet = 0.9144m. -// compressible: An indicator that distinguishes density base from pressure base. 0-incompressible, 1-compressible -// isUnsteady: An indicator that distinguishes unsteady problem from steady problem. 0-steady, 1-unsteady -// startTime: The initial time of the unsteady simulation. -// endTime: The end time of the unsteady simulation. -// dt: The time interval of the unsteady simulation. -// innerIter: The number of step for current time. -// OutputTimeStep: The interval step of output for unsteady simulation. - -int nIsComputeWallDist = 1; -string gridfile = "./grid/back.fts"; -int maxSimuStep = 2000; -int intervalStepFlow = 2000; -int intervalStepPlot = 1000; -int intervalStepRes = 10; - -double gridScaleFactor = 1.0; - -int compressible = 0; -int iunsteady = 0; -double startTime = 0.0; -double endTime = 30; -double dt = 0.1; -int innerIter = 10; -int OutputTimeStep = 5; - -######################################################################### -# Post-Processing # -######################################################################### -// nVisualVariables: Number of variables want to be dumped for tecplot visualization. -// visualVariables : Variable types dumped, listed as following: -// -- U(22), V(23), W(24), P(25), CP(26), T(27), DEN(28), VIS(29), TE(31), ED(32), enthalpy(70) -// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! -// Variables order must from small to big. - -int nVisualVariables = 4; -int visualVariables[] = [22, 23, 24, 25]; - -######################################################################### -# Flow Parameter # -######################################################################### -string FLOW[] = "FLOW"; - -// Initial value of variables or constant -double initRho = 1.0; -double initMu = 0.0001; -double initU = 0.9191874; -double initV = 0; -double initW = 0; -double initP = 0; - -// Relaxing factor -double urfU = 0.4; -double urfV = 0.4; -double urfW = 0.4; -double urfP = 0.3; -double urfFlux = 0.4; - -// Tolerance for governing equations -double resU = 1e-6; -double resV = 1e-6; -double resW = 1e-5; -double resP = 1e-5; - -// Solver for solving linear system -// : CGS/GMRES/BiCGSTAB/AMG -string iterSolvU = "BiCGSTAB"; -string iterSolvV = "BiCGSTAB"; -string iterSolvW = "BiCGSTAB"; -string iterSolvP = "AMG"; - -// Max Iter for solving linear system -int maxSweepU = 30; -int maxSweepV = 30; -int maxSweepW = 30; -int maxSweepP = 30; - -// Tolerance for solving linear system -double iterSolvTolU = 1e-3; -double iterSolvTolV = 1e-3; -double iterSolvTolW = 1e-3; -double iterSolvTolP = 1e-2; - -// Gradient Calculation -// : GAUSS/LSQ -string UGradCalc = "GAUSS"; -string VGradCalc = "GAUSS"; -string WGradCalc = "GAUSS"; -string PGradCalc = "GAUSS"; - -// Convection scheme -// : UPWIND/CDS/QUICK/SUDS -string flowConvCalc = "UPWIND"; - -// Diffusion scheme(central difference) -// : NON_ORTHOGONAL -string flowDiffCalc = "NON_ORTHOGONAL"; - -// Transient scheme -// : CRANK_NICOLSON/IMPLICIT_2ND_ORDER/IMPLICIT_EULER -string flowTranCalc = "IMPLICIT_EULER"; - -// Source for flow -// : FLOW_DEFAULT/FLOW_GRAVITY -string flowSourceCalc[] = "FLOW_DEFAULT"; - -//string flowSourceCalc[] = "FLOW_DEFAULT FLOW_GRAVITY"; -int bodyForceFlag = 0; -//double gravityX = 0.0; -//double gravityY = -9.81; -//double gravityZ = 0.0; -int isBoussinesq = 0; -######################################################################### -# Turbulence Parameter # -######################################################################### -// turb SA -//int viscousType = 11; //SPALART_ALLMARAS = 11, KEPSILON = 13 -string TURB_SA[] = ["TURB_SA"]; -string TURB_SA_SCALAR_NAME[] = ["kinetic"]; -double urfMu = 1.0; - -double kineticInitValue = 1.0; -string kineticConvCalc = "UPWIND"; -string kineticDiffCalc = "NON_ORTHOGONAL"; -string kineticSourceCalc[] = "TURB_SA_DEFAULT"; -double kineticUrf = 1.0; -double kineticRes = 1e-6; - -string turbIterSolv = "BiCGSTAB"; -int turbMaxSweep = 30; -double turbIterSolvTol = 1e-12; - - -// turb K-EPSILON -//int viscousType = 13; //SPALART_ALLMARAS = 11, KEPSILON = 13 -string TURB_K_EPSILON[] = ["TURB_K","TURB_EPSILON"]; -string TURB_K_EPSILON_SCALAR_NAME[] = ["kinetic", "epsilon - -string turbIterSolv = "BiCGSTAB"; -int turbMaxSweep = 30; -double turbIterSolvTol = 1e-12; - -string TURB_K[] = ["TURB_K"]; -string TURB_K_SCALAR_NAME[] = ["kinetic"]; -string TURB_EPSILON[] = ["TURB_EPSILON"]; -string TURB_EPSILON_SCALAR_NAME[] = ["epsilon"]; -double urfMu = 1.0; - -// turb k -double kineticInitValue = 15.48; -string kineticConvCalc = "UPWIND"; -string kineticDiffCalc = "NON_ORTHOGONAL"; -string kineticSourceCalc[] = "TURB_K_DEFAULT"; -double kineticUrf = 0.6; -double kineticRes = 1e-6; - -// turb epsilon -double epsilonInitValue = 200.3; -string epsilonConvCalc = "UPWIND"; -string epsilonDiffCalc = "NON_ORTHOGONAL"; -string epsilonSourceCalc[] = "TURB_EPSILON_DEFAULT"; -double epsilonUrf = 0.6; -double epsilonRes = 1e-6; - -######################################################################### -# Energy Parameter # -######################################################################### -// energyType: The energy solver switch. 0-off, 1-on -// ENERGY[]: Solver binding for factory mode. -// ENERGY_SCALAR_NAME[]: The name of variable to be solved in energy equation. -// energyPrintName[]: The output on the screen during the solution. - -int energyType = 0; -string ENERGY[] = ["ENERGY"]; -string ENERGY_SCALAR_NAME[] = "enthalpy"; -string energyPrintName[] = ["H"]; - -// Initial value of variables or constant -double initT = 273.0; -double initK = 0.026; -double initCPg = 1007.0; -double urfT = 0.8; -double urfH = 0.7; -double enthalpyInitValue = 0.21; - -// Discrete schemes -string energyConvCalc = "UPWIND"; -string energyDiffCalc = "NON_ORTHOGONAL"; -string energySourceCalc[] = ["EMPTY"]; -string energyGradCalc = "GAUSS"; -string energyTranCalc = "IMPLICIT_EULER"; - -// Set for solving linear equations -string enthalpyIterSolv = "BiCGSTAB"; -int enthalpyMaxSweep = 30; -double enthalpyIterSolvTol = 1e-12; -double enthalpyRes = 1e-6; \ No newline at end of file diff --git a/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/grid_para.hypara b/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/grid_para.hypara deleted file mode 100644 index 8a3018f..0000000 --- a/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/grid_para.hypara +++ /dev/null @@ -1,30 +0,0 @@ -######################################################################### -# Grid data type # -######################################################################### -// gridtype: Grid type for generation, conversion, reconstruction, merging. -// 0 -- Unstructured grid. -// 1 -- Structured grid. -// axisup: Type of Cartisien coordinates system, used in grid conversion. -// 1 -- Y upward. (default) -// 2 -- Z upward. -// from_gtype: Type of grid data type in grid conversion process. -// -1 -- MULTI_TYPE. -// 1 -- PHengLEI, *.fts. -// 2 -- CGNS, *.cgns. -// 3 -- Plot3D type of structured grid, *.dat/*.grd. -// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. -// 5 -- Fluent, *.cas/*.msh. -// 6 -- Ustar, mgrid.in. -// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. -// 8 -- GMSH, *.msh. -int gridtype = 0; -int axisup = 1; -int from_gtype = 5; - -######################################################################### -# File path # -######################################################################### -// from_gfile: path of original data file for unstructure grid convert from. -// out_gfile: path of target file for grid convert to, *.fts type of file usually. -string from_gfile = "./grid/back.cas"; -string out_gfile = "./grid/back.fts"; diff --git a/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/key.hypara b/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/key.hypara deleted file mode 100644 index dc4eed2..0000000 --- a/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/bin/key.hypara +++ /dev/null @@ -1,52 +0,0 @@ -string title = "PHengLEI Main Parameter Control File"; - -// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE. -string defaultParaFile = "./bin/cfd_para.hypara"; - -// ndim: Dimensional of the grid, 2 or 3. -// nparafile: the number of parameter files. -// nsimutask: simulation task type. -// 0 -- CFD Solver of NS or Turbulation. -// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc. -// Grid conversion: from other format to PHengLEI format (.fts). -// Grid reconstruction: such as grid adaptation. -// Grid merging: merge two blocks into one block. -// Grid repairing: repair the original grid in order to remove the negative volume cells. -// 2 -- Wall distance computation for turb-solver. -// 3 -- Grid partition. -int ndim = 2; -int nparafile = 1; - -int nsimutask = 0; -string parafilename = "./bin/cfd_para_incompressible.hypara" -//string parafilename = "./bin/cfd_para_subsonic.hypara"; -//string parafilename = "./bin/cfd_para_transonic.hypara"; -//string parafilename = "./bin/cfd_para_supersonic.hypara"; -//string parafilename = "./bin/cfd_para_hypersonic.hypara"; - -//int nsimutask = 1; -//string parafilename = "./bin/grid_para.hypara"; - -//int nsimutask = 2; -//string parafilename = "./bin/cfd_para.hypara"; - -//int nsimutask = 3; -//string parafilename = "./bin/partition.hypara"; - -//int nsimutask = 1; -//string parafilename = "./bin/grid_deform_para.hypara"; - -//int nsimutask = 1; -//string parafilename = "./bin/grid_refine_para.hypara"; - -//int nsimutask = 14; -//string parafilename = "./bin/integrative_solver.hypara"; - -//int nsimutask = 99; -//string parafilename = "./bin/post_processing.hypara"; - -// ---------------- Advanced Parameters, DO NOT care it ---------------- -int numberOfGridProcessor = 0; -// ATP read -//@string parafilename1 = "" -//@string parafilename2 = ""; \ No newline at end of file diff --git a/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/grid/网格地址.txt b/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/grid/网格地址.txt deleted file mode 100644 index 899f977..0000000 --- a/H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU/grid/网格地址.txt +++ /dev/null @@ -1,5 +0,0 @@ -红山开源风雷算例库原始网格获取百度网盘链接： -链接：http://pan.baidu.com/s/1aZ9cdkp6CkT9il4fEpnTcA -提取码：w47m - -注：plot3D格式网格需同时下载.grd和.inp文件 \ No newline at end of file diff --git a/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/boundary_condition_ref.hypara b/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/boundary_condition_ref.hypara deleted file mode 100644 index ab8c3f3..0000000 --- a/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/boundary_condition_ref.hypara +++ /dev/null @@ -1,73 +0,0 @@ -# nBoundaryConditions: Number of global boundary conditions. -# bcName : Boundary condition name. -# bcType(in PHengLEI): Boundary condition type. - -# How to set boundary condition, for example: -# string bcName = "Wall"; -# { -# int bcType = 2; -# int viscousType = 1; -# double wallTemperature = -1.0; -# double uWall = 0.0; -# double vWall = 0.0; -# double wWall = 0.0; -# } -# string bcName = "Inflow"; -# { -# int bcType = 5; -# int inflowParaType = 0; -# double refMachNumber = 0.73; -# double attackd = 2.79; -# double angleSlide = 0.0; -# double refReNumber = 6.5e6; -# double refDimensionalTemperature = 288.15; -# } - -# For more information, see examples/bin/boundary_condition.hypara file!!! - -int nBoundaryConditions = 4; -string bcName = "bottomwall"; -{ - string bodyName = "body"; - int bcType = 2; - string flowType = "FLOW_SOLID_SURFACE"; - string energyBoundaryType = "ENERGY_WALL"; -} -string bcName = "coldwall"; -{ - string bodyName = "body"; - int bcType = 2; - string flowType = "FLOW_SOLID_SURFACE"; - string energyBoundaryType = "ENERGY_WALL"; - double T = 290.0; -} -string bcName = "hotwall"; -{ - string bodyName = "body"; - int bcType = 2; - string flowType = "FLOW_SOLID_SURFACE"; - string energyBoundaryType = "ENERGY_WALL"; - double T = 305.0; -} -string bcName = "topwall"; -{ - string bodyName = "body"; - int bcType = 2; - string flowType = "FLOW_SOLID_SURFACE"; - string energyBoundaryType = "ENERGY_WALL"; -} - -# 'bcType' is defined as following: -# -2: WAKE -# -1: INTERFACE -# 0 : NO_BOUNDARY_CONDITION -# 1 : EXTRAPOLATION -# 2 : SOLID_SURFACE -# 3 : SYMMETRY -# 4 : FARFIELD -# 5 : INFLOW -# 6 : OUTFLOW -# 52: PRESSURE_INLET -# 62: PRESSURE_OUTLET -# 61: OUTFLOW_CONFINED -# 7 : POLE diff --git a/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/cfd_para_incompressible.hypara b/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/cfd_para_incompressible.hypara deleted file mode 100644 index e51c789..0000000 --- a/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/cfd_para_incompressible.hypara +++ /dev/null @@ -1,214 +0,0 @@ -######################################################################### -# General Control Parameter # -######################################################################### -// nIsComputeWallDist: Whether to compute the wall distance. -// 0 -- Compute wall distance. -// 1 -- Not compute. -// gridfile: The partitioned Grid file path, using relative path, -// which is relative to the working directory. -// maxSimuStep: The max simulation step, don't care simulation is restart or not. -// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. -// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. -// intervalStepRes: The step intervals for residual 'res.dat' saved. -// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like: -// 1 dm = 0.1 m. -// 1 cm = 0.01 m. -// 1 mm = 0.001m. -// 1 inch = 0.0254m. -// 1 foot = 12 inches = 0.3048m. -// 1 yard = 3 feet = 0.9144m. -// compressible: An indicator that distinguishes density base from pressure base. 0-incompressible, 1-compressible -// isUnsteady: An indicator that distinguishes unsteady problem from steady problem. 0-steady, 1-unsteady -// startTime: The initial time of the unsteady simulation. -// endTime: The end time of the unsteady simulation. -// dt: The time interval of the unsteady simulation. -// innerIter: The number of step for current time. -// OutputTimeStep: The interval step of output for unsteady simulation. - -int nIsComputeWallDist = 1; -string gridfile = "./grid/run.fts"; -int maxSimuStep = 10000; -int intervalStepFlow = 2000; -int intervalStepPlot = 1000; -int intervalStepRes = 10; - -double gridScaleFactor = 1.0; - -int compressible = 0; -int iunsteady = 0; -double startTime = 0.0; -double endTime = 20.0; -double dt = 0.1; -int innerIter = 10; -int OutputTimeStep = 5; - -######################################################################### -# Post-Processing # -######################################################################### -// nVisualVariables: Number of variables want to be dumped for tecplot visualization. -// visualVariables : Variable types dumped, listed as following: -// -- U(22), V(23), W(24), P(25), CP(26), T(27), DEN(28), VIS(29), TE(31), ED(32), enthalpy(70) -// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! -// Variables order must from small to big. - -int nVisualVariables = 6; -int visualVariables[] = [22, 23, 24, 25, 27, 70]; - -######################################################################### -# Flow Parameter # -######################################################################### -string FLOW[] = "FLOW"; - -// Initial value of variables or constant -double initRho = 1.1405; -double initMu = 1.7894e-5; -double initU = 0; -double initV = 0; -double initW = 0; -double initP = 0; - -// Relaxing factor -double urfU = 0.7; -double urfV = 0.7; -double urfW = 0.7; -double urfP = 0.3; -double urfFlux = 0.0; - -// Tolerance for governing equations -double resU = 1e-6; -double resV = 1e-6; -double resW = 1e-5; -double resP = 1e-5; - -// Solver for solving linear system -// : CGS/GMRES/BiCGSTAB/AMG -string iterSolvU = "BiCGSTAB"; -string iterSolvV = "BiCGSTAB"; -string iterSolvW = "BiCGSTAB"; -string iterSolvP = "GMRES"; - -// Max Iter for solving linear system -int maxSweepU = 30; -int maxSweepV = 30; -int maxSweepW = 30; -int maxSweepP = 30; - -// Tolerance for solving linear system -double iterSolvTolU = 1e-3; -double iterSolvTolV = 1e-3; -double iterSolvTolW = 1e-3; -double iterSolvTolP = 1e-2; - -// Gradient Calculation -// : GAUSS/LSQ -string UGradCalc = "GAUSS"; -string VGradCalc = "GAUSS"; -string WGradCalc = "GAUSS"; -string PGradCalc = "GAUSS"; - -// Convection scheme -// : UPWIND/CDS/QUICK/SUDS -string flowConvCalc = "UPWIND"; - -// Diffusion scheme(central difference) -// : NON_ORTHOGONAL -string flowDiffCalc = "NON_ORTHOGONAL"; - -// Transient scheme -// : CRANK_NICOLSON/IMPLICIT_2ND_ORDER/IMPLICIT_EULER -string flowTranCalc = "IMPLICIT_EULER"; - -// Source for flow -// : FLOW_DEFAULT/FLOW_GRAVITY -//string flowSourceCalc[] = "FLOW_DEFAULT"; - -string flowSourceCalc[] = "FLOW_DEFAULT FLOW_GRAVITY"; -int bodyForceFlag = 1; -double gravityX = 0.0; -double gravityY = -9.81; -double gravityZ = 0.0; -int isBoussinesq = 1; -double thermalExpansion = 3.44827e-3; -double refT = 290; - -######################################################################### -# Turbulence Parameter # -######################################################################### -//int viscousType = 13; //SPALART_ALLMARAS = 11, KEPSILON = 13 - -//turb SA -string TURB_SA[] = ["TURB_SA"]; -string TURB_SA_SCALAR_NAME[] = ["kinetic"]; -double urfMu = 1.0; - -double kineticInitValue = 1.0; -string kineticConvCalc = "UPWIND"; -string kineticDiffCalc = "NON_ORTHOGONAL"; -string kineticSourceCalc[] = "TURB_SA_DEFAULT"; -double kineticUrf = 1.0; -double kineticRes = 1e-6; - -string turbIterSolv = "BiCGSTAB"; -int turbMaxSweep = 30; -double turbIterSolvTol = 1e-12; - - -//turb KEPSILON -string TURB_K_EPSILON[] = ["TURB_K","TURB_EPSILON"]; -string TURB_K_EPSILON_SCALAR_NAME[] = ["kinetic", "epsilon"]; - -string TURB_K[] = ["TURB_K"]; -string TURB_K_SCALAR_NAME[] = ["kinetic"]; -string TURB_EPSILON[] = ["TURB_EPSILON"]; -string TURB_EPSILON_SCALAR_NAME[] = ["epsilon"]; -double urfMu = 1.0; - -// turb k -double kineticInitValue = 1.0; -string kineticConvCalc = "UPWIND"; -string kineticDiffCalc = "NON_ORTHOGONAL"; -string kineticSourceCalc[] = "TURB_K_DEFAULT"; -double kineticUrf = 1.0; -double kineticRes = 1e-6; - -// turb epsilon -double epsilonInitValue = 1.0; -string epsilonConvCalc = "UPWIND"; -string epsilonDiffCalc = "NON_ORTHOGONAL"; -string epsilonSourceCalc[] = "TURB_EPSILON_DEFAULT"; -double epsilonUrf = 1.0; -double epsilonRes = 1e-6; - -######################################################################### -# Energy Parameter # -######################################################################### -// energyType: The energy solver switch. 0-off, 1-on -// ENERGY[]: Solver binding for factory mode. -// ENERGY_SCALAR_NAME[]: The name of variable to be solved in energy equation. -// energyPrintName[]: The output on the screen during the solution. - -int energyType = 1; -string ENERGY[] = ["ENERGY"]; -string ENERGY_SCALAR_NAME[] = "enthalpy"; -string energyPrintName[] = ["H"]; - -// Initial value of variables or constant -double initT = 295; -double initK = 0.0242; -double initCPg = 1006.43; -double urfT = 0.2; -double urfH = 0.2; -double enthalpyInitValue = 0.21; - -// Discrete schemes -string energyConvCalc = "UPWIND"; -string energyDiffCalc = "NON_ORTHOGONAL"; -string energySourceCalc[] = ["EMPTY"]; -string energyGradCalc = "GAUSS"; -string energyTranCalc = "IMPLICIT_EULER"; - -// Set for solving linear equations -string enthalpyIterSolv = "BiCGSTAB"; -int enthalpyMaxSweep = 30; -double enthalpyIterSolvTol = 1e-12; -double enthalpyRes = 1e-6; \ No newline at end of file diff --git a/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/grid_para.hypara b/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/grid_para.hypara deleted file mode 100644 index b66d187..0000000 --- a/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/grid_para.hypara +++ /dev/null @@ -1,30 +0,0 @@ -######################################################################### -# Grid data type # -######################################################################### -// gridtype: Grid type for generation, conversion, reconstruction, merging. -// 0 -- Unstructured grid. -// 1 -- Structured grid. -// axisup: Type of Cartisien coordinates system, used in grid conversion. -// 1 -- Y upward. (default) -// 2 -- Z upward. -// from_gtype: Type of grid data type in grid conversion process. -// -1 -- MULTI_TYPE. -// 1 -- PHengLEI, *.fts. -// 2 -- CGNS, *.cgns. -// 3 -- Plot3D type of structured grid, *.dat/*.grd. -// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. -// 5 -- Fluent, *.cas/*.msh. -// 6 -- Ustar, mgrid.in. -// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. -// 8 -- GMSH, *.msh. -int gridtype = 0; -int axisup = 1; -int from_gtype = 5; - -######################################################################### -# File path # -######################################################################### -// from_gfile: path of original data file for unstructure grid convert from. -// out_gfile: path of target file for grid convert to, *.fts type of file usually. -string from_gfile = "./grid/run.cas"; -string out_gfile = "./grid/run.fts"; diff --git a/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/grid/网格地址.txt b/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/grid/网格地址.txt deleted file mode 100644 index 899f977..0000000 --- a/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/grid/网格地址.txt +++ /dev/null @@ -1,5 +0,0 @@ -红山开源风雷算例库原始网格获取百度网盘链接： -链接：http://pan.baidu.com/s/1aZ9cdkp6CkT9il4fEpnTcA -提取码：w47m - -注：plot3D格式网格需同时下载.grd和.inp文件 \ No newline at end of file diff --git a/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/boundary_condition_ref.hypara b/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/boundary_condition_ref.hypara deleted file mode 100644 index 5666545..0000000 --- a/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/boundary_condition_ref.hypara +++ /dev/null @@ -1,68 +0,0 @@ -# nBoundaryConditions: Number of global boundary conditions. -# bcName : Boundary condition name. -# bcType(in PHengLEI): Boundary condition type. - -# How to set boundary condition, for example: -# string bcName = "Wall"; -# { -# int bcType = 2; -# int viscousType = 1; -# double wallTemperature = -1.0; -# double uWall = 0.0; -# double vWall = 0.0; -# double wWall = 0.0; -# } -# string bcName = "Inflow"; -# { -# int bcType = 5; -# int inflowParaType = 0; -# double refMachNumber = 0.73; -# double attackd = 2.79; -# double angleSlide = 0.0; -# double refReNumber = 6.5e6; -# double refDimensionalTemperature = 288.15; -# } - -# For more information, see examples/bin/boundary_condition.hypara file!!! - -int nBoundaryConditions = 4; -string bcName = "bottom"; -{ - string bodyName = "body"; - int bcType = 2; - string flowType = "FLOW_SOLID_SURFACE"; -} -string bcName = "left"; -{ - string bodyName = "body"; - int bcType = 2; - string flowType = "FLOW_SOLID_SURFACE"; -} -string bcName = "right"; -{ - string bodyName = "body"; - int bcType = 2; - string flowType = "FLOW_SOLID_SURFACE"; -} -string bcName = "top"; -{ - string bodyName = "body"; - int bcType = 2; - string flowType = "FLOW_SOLID_SURFACE"; - double flowU = 1.0; -} - -# 'bcType' is defined as following: -# -2: WAKE -# -1: INTERFACE -# 0 : NO_BOUNDARY_CONDITION -# 1 : EXTRAPOLATION -# 2 : SOLID_SURFACE -# 3 : SYMMETRY -# 4 : FARFIELD -# 5 : INFLOW -# 6 : OUTFLOW -# 52: PRESSURE_INLET -# 62: PRESSURE_OUTLET -# 61: OUTFLOW_CONFINED -# 7 : POLE diff --git a/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/cfd_para_incompressible.hypara b/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/cfd_para_incompressible.hypara deleted file mode 100644 index 5f04ee5..0000000 --- a/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/cfd_para_incompressible.hypara +++ /dev/null @@ -1,197 +0,0 @@ -######################################################################### -# General Control Parameter # -######################################################################### -// nIsComputeWallDist: Whether to compute the wall distance. -// 0 -- Compute wall distance. -// 1 -- Not compute. -// gridfile: The partitioned Grid file path, using relative path, -// which is relative to the working directory. -// maxSimuStep: The max simulation step, don't care simulation is restart or not. -// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. -// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. -// intervalStepRes: The step intervals for residual 'res.dat' saved. -// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like: -// 1 dm = 0.1 m. -// 1 cm = 0.01 m. -// 1 mm = 0.001m. -// 1 inch = 0.0254m. -// 1 foot = 12 inches = 0.3048m. -// 1 yard = 3 feet = 0.9144m. -// compressible: An indicator that distinguishes density base from pressure base. 0-incompressible, 1-compressible -// isUnsteady: An indicator that distinguishes unsteady problem from steady problem. 0-steady, 1-unsteady -// startTime: The initial time of the unsteady simulation. -// endTime: The end time of the unsteady simulation. -// dt: The time interval of the unsteady simulation. -// innerIter: The number of step for current time. -// OutputTimeStep: The interval step of output for unsteady simulation. - -int nIsComputeWallDist = 1; -string gridfile = "./grid/cavity.fts"; -int maxSimuStep = 10000; -int intervalStepFlow = 2000; -int intervalStepPlot = 2000; -int intervalStepRes = 10; - -double gridScaleFactor = 1.0; - -int compressible = 0; -int iunsteady = 0; -double startTime = 0.0; -double endTime = 30; -double dt = 0.1; -int innerIter = 10; -int OutputTimeStep = 5; - -######################################################################### -# Post-Processing # -######################################################################### -// nVisualVariables: Number of variables want to be dumped for tecplot visualization. -// visualVariables : Variable types dumped, listed as following: -// -- U(22), V(23), W(24), P(25), CP(26), T(27), DEN(28), VIS(29), TE(31), ED(32), enthalpy(70) -// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! -// Variables order must from small to big. - -int nVisualVariables = 4; -int visualVariables[] = [22, 23, 24, 25]; -######################################################################### -# Flow Parameter # -######################################################################### -string FLOW[] = "FLOW"; - -// Initial value of variables or constant -double initRho = 1.0; -double initMu = 0.001; -double initU = 0; -double initV = 0; -double initW = 0; -double initP = 0; - -// Relaxing factor -double urfU = 0.4; -double urfV = 0.4; -double urfW = 0.4; -double urfP = 0.7; -double urfFlux = 0.4; - -// Tolerance for governing equations -double resU = 1e-6; -double resV = 1e-6; -double resW = 1e-5; -double resP = 1e-5; - -// Solver for solving linear system -// : CGS/GMRES/BiCGSTAB/AMG -string iterSolvU = "BiCGSTAB"; -string iterSolvV = "BiCGSTAB"; -string iterSolvW = "BiCGSTAB"; -string iterSolvP = "GMRES"; - -// Max Iter for solving linear system -int maxSweepU = 30; -int maxSweepV = 30; -int maxSweepW = 30; -int maxSweepP = 30; - -// Tolerance for solving linear system -double iterSolvTolU = 1e-3; -double iterSolvTolV = 1e-3; -double iterSolvTolW = 1e-3; -double iterSolvTolP = 1e-2; - -// Gradient Calculation -// : GAUSS/LSQ -string UGradCalc = "GAUSS"; -string VGradCalc = "GAUSS"; -string WGradCalc = "GAUSS"; -string PGradCalc = "GAUSS"; - -// Convection scheme -// : UPWIND/CDS/QUICK/SUDS -string flowConvCalc = "UPWIND"; - -// Diffusion scheme(central difference) -// : NON_ORTHOGONAL -string flowDiffCalc = "NON_ORTHOGONAL"; - -// Transient scheme -// : CRANK_NICOLSON/IMPLICIT_2ND_ORDER/IMPLICIT_EULER -string flowTranCalc = "IMPLICIT_EULER"; - -// Source for flow -// : FLOW_DEFAULT/FLOW_GRAVITY -string flowSourceCalc[] = "FLOW_DEFAULT"; - -// string flowSourceCalc[] = "FLOW_DEFAULT FLOW_GRAVITY"; -int bodyForceFlag = 0; -int isBoussinesq = 0; -//double gravityX = 0.0; -//double gravityY = -9.81; -//double gravityZ = 0.0; - -######################################################################### -# Turbulence Parameter # -######################################################################### -// turb K-EPSILON -//int viscousType = 13; //SPALART_ALLMARAS = 11, KEPSILON = 13 -string TURB_K_EPSILON[] = ["TURB_K","TURB_EPSILON"]; -string TURB_K_EPSILON_SCALAR_NAME[] = ["kinetic", "epsilon"]; - -string turbIterSolv = "BiCGSTAB"; -int turbMaxSweep = 30; -double turbIterSolvTol = 1e-12; - -string TURB_K[] = ["TURB_K"]; -string TURB_K_SCALAR_NAME[] = ["kinetic"]; -string TURB_EPSILON[] = ["TURB_EPSILON"]; -string TURB_EPSILON_SCALAR_NAME[] = ["epsilon"]; -double urfMu = 1.0; - -// turb k -double kineticInitValue = 1.0; -string kineticConvCalc = "UPWIND"; -string kineticDiffCalc = "NON_ORTHOGONAL"; -string kineticSourceCalc[] = "TURB_K_DEFAULT"; -double kineticUrf = 1.0; -double kineticRes = 1e-6; - -// turb epsilon -double epsilonInitValue = 1.0; -string epsilonConvCalc = "UPWIND"; -string epsilonDiffCalc = "NON_ORTHOGONAL"; -string epsilonSourceCalc[] = "TURB_EPSILON_DEFAULT"; -double epsilonUrf = 1.0; -double epsilonRes = 1e-6; - -######################################################################### -# Energy Parameter # -######################################################################### -// energyType: The energy solver switch. 0-off, 1-on -// ENERGY[]: Solver binding for factory mode. -// ENERGY_SCALAR_NAME[]: The name of variable to be solved in energy equation. -// energyPrintName[]: The output on the screen during the solution. - -int energyType = 0; -string ENERGY[] = ["ENERGY"]; -string ENERGY_SCALAR_NAME[] = "enthalpy"; -string energyPrintName[] = ["H"]; - -// Initial value of variables or constant -double initT = 273.0; -double initK = 0.026; -double initCPg = 1007.0; -double urfT = 0.8; -double urfH = 0.7; -double enthalpyInitValue = 0.21; - -// Discrete schemes -string energyConvCalc = "UPWIND"; -string energyDiffCalc = "NON_ORTHOGONAL"; -string energySourceCalc[] = ["EMPTY"]; -string energyGradCalc = "GAUSS"; -string energyTranCalc = "IMPLICIT_EULER"; - -// Set for solving linear equations -string enthalpyIterSolv = "BiCGSTAB"; -int enthalpyMaxSweep = 30; -double enthalpyIterSolvTol = 1e-12; -double enthalpyRes = 1e-6; \ No newline at end of file diff --git a/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/grid_para.hypara b/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/grid_para.hypara deleted file mode 100644 index b90c53e..0000000 --- a/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/grid_para.hypara +++ /dev/null @@ -1,30 +0,0 @@ -######################################################################### -# Grid data type # -######################################################################### -// gridtype: Grid type for generation, conversion, reconstruction, merging. -// 0 -- Unstructured grid. -// 1 -- Structured grid. -// axisup: Type of Cartisien coordinates system, used in grid conversion. -// 1 -- Y upward. (default) -// 2 -- Z upward. -// from_gtype: Type of grid data type in grid conversion process. -// -1 -- MULTI_TYPE. -// 1 -- PHengLEI, *.fts. -// 2 -- CGNS, *.cgns. -// 3 -- Plot3D type of structured grid, *.dat/*.grd. -// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. -// 5 -- Fluent, *.cas/*.msh. -// 6 -- Ustar, mgrid.in. -// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. -// 8 -- GMSH, *.msh. -int gridtype = 0; -int axisup = 1; -int from_gtype = 5; - -######################################################################### -# File path # -######################################################################### -// from_gfile: path of original data file for unstructure grid convert from. -// out_gfile: path of target file for grid convert to, *.fts type of file usually. -string from_gfile = "./grid/cavity.cas"; -string out_gfile = "./grid/cavity.fts"; diff --git a/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/grid/网格地址.txt b/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/grid/网格地址.txt deleted file mode 100644 index 899f977..0000000 --- a/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/grid/网格地址.txt +++ /dev/null @@ -1,5 +0,0 @@ -红山开源风雷算例库原始网格获取百度网盘链接： -链接：http://pan.baidu.com/s/1aZ9cdkp6CkT9il4fEpnTcA -提取码：w47m - -注：plot3D格式网格需同时下载.grd和.inp文件 \ No newline at end of file diff --git a/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/boundary_condition_ref.hypara b/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/boundary_condition_ref.hypara deleted file mode 100644 index 9cf8c2f..0000000 --- a/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/boundary_condition_ref.hypara +++ /dev/null @@ -1,71 +0,0 @@ -# nBoundaryConditions: Number of global boundary conditions. -# bcName : Boundary condition name. -# bcType(in PHengLEI): Boundary condition type. - -# How to set boundary condition, for example: -# string bcName = "Wall"; -# { -# int bcType = 2; -# int viscousType = 1; -# double wallTemperature = -1.0; -# double uWall = 0.0; -# double vWall = 0.0; -# double wWall = 0.0; -# } -# string bcName = "Inflow"; -# { -# int bcType = 5; -# int inflowParaType = 0; -# double refMachNumber = 0.73; -# double attackd = 2.79; -# double angleSlide = 0.0; -# double refReNumber = 6.5e6; -# double refDimensionalTemperature = 288.15; -# } - -# For more information, see examples/bin/boundary_condition.hypara file!!! - -int nBoundaryConditions = 3; -string bcName = "in"; -{ - int bcType = 5; - string flowType = "FLOW_VELOCITY_INLET"; - string kineticBoundaryType = "TURB_K_INLET"; - string epsilonBoundaryType = "TURB_EPSILON_INLET"; - double flowW = 50; - double kinetic = 9.375004; - double epsilon = 54151.86; -} -string bcName = "out"; -{ - int bcType = 6; - string flowType = "FLOW_PRESSURE_OUTLET"; - string kineticBoundaryType = "TURB_K_PRESSUREOUTLET"; - string epsilonBoundaryType = "TURB_EPSILON_PRESSUREOUTLET"; - double flowP = 0; - double kinetic = 9.375004; - double epsilon = 54151.86; -} -string bcName = "wall"; -{ - string bodyName = "body"; - int bcType = 2; - string flowType = "FLOW_SOLID_SURFACE"; - string kineticBoundaryType = "TURB_K_WALL"; - string epsilonBoundaryType = "TURB_EPSILON_WALL"; -} - -# 'bcType' is defined as following: -# -2: WAKE -# -1: INTERFACE -# 0 : NO_BOUNDARY_CONDITION -# 1 : EXTRAPOLATION -# 2 : SOLID_SURFACE -# 3 : SYMMETRY -# 4 : FARFIELD -# 5 : INFLOW -# 6 : OUTFLOW -# 52: PRESSURE_INLET -# 62: PRESSURE_OUTLET -# 61: OUTFLOW_CONFINED -# 7 : POLE diff --git a/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/cfd_para_incompressible.hypara b/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/cfd_para_incompressible.hypara deleted file mode 100644 index 3048a1c..0000000 --- a/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/cfd_para_incompressible.hypara +++ /dev/null @@ -1,202 +0,0 @@ -######################################################################### -# General Control Parameter # -######################################################################### -// nIsComputeWallDist: Whether to compute the wall distance. -// 0 -- Compute wall distance. -// 1 -- Not compute. -// gridfile: The partitioned Grid file path, using relative path, -// which is relative to the working directory. -// maxSimuStep: The max simulation step, don't care simulation is restart or not. -// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. -// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. -// intervalStepRes: The step intervals for residual 'res.dat' saved. -// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like: -// 1 dm = 0.1 m. -// 1 cm = 0.01 m. -// 1 mm = 0.001m. -// 1 inch = 0.0254m. -// 1 foot = 12 inches = 0.3048m. -// 1 yard = 3 feet = 0.9144m. -// compressible: An indicator that distinguishes density base from pressure base. 0-incompressible, 1-compressible -// isUnsteady: An indicator that distinguishes unsteady problem from steady problem. 0-steady, 1-unsteady -// startTime: The initial time of the unsteady simulation. -// endTime: The end time of the unsteady simulation. -// dt: The time interval of the unsteady simulation. -// innerIter: The number of step for current time. -// OutputTimeStep: The interval step of output for unsteady simulation. - -int nIsComputeWallDist = 1; -string gridfile = "./grid/pipe.fts"; -int maxSimuStep = 10000; -int intervalStepFlow = 1000; -int intervalStepPlot = 1000; -int intervalStepRes = 1000; - -double gridScaleFactor = 1; - -int compressible = 0; -int iunsteady = 0; -double startTime = 0.0; -double endTime = 5; -double dt = 0.1; -int innerIter = 10; -int OutputTimeStep = 5; - -######################################################################### -# Post-Processing # -######################################################################### -// nVisualVariables: Number of variables want to be dumped for tecplot visualization. -// visualVariables : Variable types dumped, listed as following: -// -- U(22), V(23), W(24), P(25), CP(26), T(27), DEN(28), VIS(29), TE(31), ED(32), enthalpy(57) -// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! -// Variables order must from small to big. -// plotFieldType: If dump out the field results to visulization. - -int plotFieldType = 1; -//int nVisualVariables = 4; -//int visualVariables[] = [22, 23, 24, 25]; - -int nVisualVariables = 7; -int visualVariables[] = [22, 23, 24, 25, 29,31,32]; -######################################################################### -# Flow Parameter # -######################################################################### -string FLOW[] = "FLOW"; - -// Initial value of variables or constant -double initRho = 1.225; -double initMu = 1.7894e-05; -double initU = 0; -double initV = 0; -double initW = 50; -double initP = 0; - -// Relaxing factor -double urfU = 0.4; -double urfV = 0.4; -double urfW = 0.4; -double urfP = 0.3; -double urfFlux = 0.4; - -// Tolerance for governing equations -double resU = 1e-6; -double resV = 1e-6; -double resW = 1e-5; -double resP = 1e-5; - -// Solver for solving linear system -// : CGS/GMRES/BiCGSTAB/AMG -string iterSolvU = "BiCGSTAB"; -string iterSolvV = "BiCGSTAB"; -string iterSolvW = "BiCGSTAB"; -string iterSolvP = "AMG"; - -// Max Iter for solving linear system -int maxSweepU = 30; -int maxSweepV = 30; -int maxSweepW = 30; -int maxSweepP = 30; - -// Tolerance for solving linear system -double iterSolvTolU = 1e-4; -double iterSolvTolV = 1e-4; -double iterSolvTolW = 1e-4; -double iterSolvTolP = 1e-3; - -// Gradient Calculation -// : GAUSS/LSQ -string UGradCalc = "GAUSS"; -string VGradCalc = "GAUSS"; -string WGradCalc = "GAUSS"; -string PGradCalc = "GAUSS"; - -// Convection scheme -// : UPWIND/CDS/QUICK/SUDS -string flowConvCalc = "UPWIND"; - -// Diffusion scheme(central difference) -// : NON_ORTHOGONAL -string flowDiffCalc = "NON_ORTHOGONAL"; - -// Transient scheme -// : CRANK_NICOLSON/IMPLICIT_2ND_ORDER/IMPLICIT_EULER -string flowTranCalc = "IMPLICIT_EULER"; - -// Source for flow -// : FLOW_DEFAULT/FLOW_GRAVITY -string flowSourceCalc[] = "FLOW_DEFAULT"; - -//string flowSourceCalc[] = "FLOW_DEFAULT FLOW_GRAVITY"; -int bodyForceFlag = 0; -double gravityX = 0.0; -double gravityY = -9.81; -double gravityZ = 0.0; - -######################################################################### -# Turbulence Parameter # -######################################################################### -int viscousType = 13; //SPALART_ALLMARAS = 11, KEPSILON = 13 - -//turb K-EPSILON -string TURB_K_EPSILON[] = ["TURB_K","TURB_EPSILON"]; -string TURB_K_EPSILON_SCALAR_NAME[] = ["kinetic", "epsilon"]; - -string TURB_K[] = ["TURB_K"]; -string TURB_K_SCALAR_NAME[] = ["kinetic"]; -string TURB_EPSILON[] = ["TURB_EPSILON"]; -string TURB_EPSILON_SCALAR_NAME[] = ["epsilon"]; -double urfMu = 0.6; - -string turbIterSolv = "BiCGSTAB"; -int turbMaxSweep = 30; -double turbIterSolvTol = 1e-12; - -// turb k -double kineticInitValue = 9.375001; -string kineticConvCalc = "UPWIND"; -string kineticDiffCalc = "NON_ORTHOGONAL"; -string kineticSourceCalc[] = "TURB_K_DEFAULT"; -double kineticUrf = 0.6; -double kineticRes = 1e-6; - - -// turb epsilon -double epsilonInitValue = 54151.86; -string epsilonConvCalc = "UPWIND"; -string epsilonDiffCalc = "NON_ORTHOGONAL"; -string epsilonSourceCalc[] = "TURB_EPSILON_DEFAULT"; -double epsilonUrf = 0.6; -double epsilonRes = 1e-6; - -######################################################################### -# Energy Parameter # -######################################################################### -// energyType: The energy solver switch. 0-off, 1-on -// ENERGY[]: Solver binding for factory mode. -// ENERGY_SCALAR_NAME[]: The name of variable to be solved in energy equation. -// energyPrintName[]: The output on the screen during the solution. -int energyType = 0; -string ENERGY[] = ["ENERGY"]; -string ENERGY_SCALAR_NAME[] = "enthalpy"; -string energyPrintName[] = ["H"]; - -// Initial value of variables or constant -double initT = 273.0; -double initK = 0.026; -double initCPg = 1007.0; -double urfT = 0.8; -double urfH = 0.7; -double enthalpyInitValue = 0.21; - -// Discrete schemes -string energyConvCalc = "UPWIND"; -string energyDiffCalc = "NON_ORTHOGONAL"; -string energySourceCalc[] = ["EMPTY"]; -string energyGradCalc = "GAUSS"; -string energyTranCalc = "IMPLICIT_EULER"; - -// Set for solving linear equations -string enthalpyIterSolv = "BiCGSTAB"; -int enthalpyMaxSweep = 30; -double enthalpyIterSolvTol = 1e-12; -double enthalpyRes = 1e-6; \ No newline at end of file diff --git a/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/grid_para.hypara b/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/grid_para.hypara deleted file mode 100644 index fc56698..0000000 --- a/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/grid_para.hypara +++ /dev/null @@ -1,30 +0,0 @@ -######################################################################### -# Grid data type # -######################################################################### -// gridtype: Grid type for generation, conversion, reconstruction, merging. -// 0 -- Unstructured grid. -// 1 -- Structured grid. -// axisup: Type of Cartisien coordinates system, used in grid conversion. -// 1 -- Y upward. (default) -// 2 -- Z upward. -// from_gtype: Type of grid data type in grid conversion process. -// -1 -- MULTI_TYPE. -// 1 -- PHengLEI, *.fts. -// 2 -- CGNS, *.cgns. -// 3 -- Plot3D type of structured grid, *.dat/*.grd. -// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. -// 5 -- Fluent, *.cas/*.msh. -// 6 -- Ustar, mgrid.in. -// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. -// 8 -- GMSH, *.msh. -int gridtype = 0; -int axisup = 1; -int from_gtype = 5; - -######################################################################### -# File path # -######################################################################### -// from_gfile: path of original data file for unstructure grid convert from. -// out_gfile: path of target file for grid convert to, *.fts type of file usually. -string from_gfile = "./grid/pipe.cas"; -string out_gfile = "./grid/pipe.fts"; diff --git a/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/grid/网格地址.txt b/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/grid/网格地址.txt deleted file mode 100644 index 899f977..0000000 --- a/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/grid/网格地址.txt +++ /dev/null @@ -1,5 +0,0 @@ -红山开源风雷算例库原始网格获取百度网盘链接： -链接：http://pan.baidu.com/s/1aZ9cdkp6CkT9il4fEpnTcA -提取码：w47m - -注：plot3D格式网格需同时下载.grd和.inp文件 \ No newline at end of file diff --git a/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/boundary_condition_ref.hypara b/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/boundary_condition_ref.hypara deleted file mode 100644 index 5bd1dce..0000000 --- a/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/boundary_condition_ref.hypara +++ /dev/null @@ -1,63 +0,0 @@ -# nBoundaryConditons : number of global boundary conditions. -# bcName : Boundary Condition Name. -# bcType(in PHengLEI): Boundary Condition Type. - -# Account of how to set boundaryconditon. -# string bcName = "Farfield"; -# { -# int bcType = 4; -# int inflowParaType = 1; -# double attackd = 0; -# double refReNumber = 6.5e6; -# double refMachNumber = 3.5; -# double angleSlide = 0; -# } - -int nBoundaryConditions = 5; -string bcName = "sym"; -{ - string bodyName = "body"; - int bcType = 2; - string flowType = "FLOW_SOLID_SURFACE"; -} -string bcName = "symf"; -{ - string bodyName = "body"; - int bcType = 2; - string flowType = "FLOW_SOLID_SURFACE"; -} -string bcName = "wall"; -{ - string bodyName = "body"; - int bcType = 2; - string flowType = "FLOW_SOLID_SURFACE"; -} -string bcName = "in"; -{ - int bcType = 5; - string flowType = "FLOW_VELOCITY_INLET"; - double flowU =0.1; -} -string bcName = "out"; -{ - int bcType = 6; - string flowType = "FLOW_PRESSURE_OUTLET"; - double flowU =0.1; - double flowP =0; -} - -# 'bcType' is defined as following: -# 99: PERIODIC -# -2: WAKE -# -1: INTERFACE -# 0 : NO_BOUNDARY_CONDITION -# 1 : EXTRAPOLATION -# 2 : SOLID_SURFACE -# 3 : SYMMETRY -# 4 : FARFIELD -# 5 : INFLOW -# 6 : OUTFLOW -# 52: PRESSURE_INLET -# 62: PRESSURE_OUTLET -# 61: OUTFLOW_CONFINED -# 7 : POLE diff --git a/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/cfd_para_incompressible.hypara b/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/cfd_para_incompressible.hypara deleted file mode 100644 index 3be1cac..0000000 --- a/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/cfd_para_incompressible.hypara +++ /dev/null @@ -1,212 +0,0 @@ -######################################################################### -# General Control Parameter # -######################################################################### -// nIsComputeWallDist: Whether to compute the wall distance. -// 0 -- Compute wall distance. -// 1 -- Not compute. -// gridfile: The partitioned Grid file path, using relative path, -// which is relative to the working directory. -// maxSimuStep: The max simulation step, don't care simulation is restart or not. -// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. -// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. -// intervalStepRes: The step intervals for residual 'res.dat' saved. -// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like: -// 1 dm = 0.1 m. -// 1 cm = 0.01 m. -// 1 mm = 0.001m. -// 1 inch = 0.0254m. -// 1 foot = 12 inches = 0.3048m. -// 1 yard = 3 feet = 0.9144m. -// compressible: An indicator that distinguishes density base from pressure base. 0-incompressible, 1-compressible -// isUnsteady: An indicator that distinguishes unsteady problem from steady problem. 0-steady, 1-unsteady -// startTime: The initial time of the unsteady simulation. -// endTime: The end time of the unsteady simulation. -// dt: The time interval of the unsteady simulation. -// innerIter: The number of step for current time. -// OutputTimeStep: The interval step of output for unsteady simulation. - -int nIsComputeWallDist = 1; -string gridfile = "./grid/suboff.fts"; -iint maxSimuStep = 10000; -int intervalStepFlow = 2000; -int intervalStepPlot = 2000; -int intervalStepRes = 2000; - -double gridScaleFactor = 1.0; - -int compressible = 0; -int iunsteady = 0; -double startTime = 0.0; -double endTime = 5; -double dt = 0.1; -int innerIter = 10; -int OutputTimeStep = 5; - -######################################################################### -# Post-Processing # -######################################################################### -// nVisualVariables: Number of variables want to be dumped for tecplot visualization. -// visualVariables : Variable types dumped, listed as following: -// -- U(22), V(23), W(24), P(25), CP(26), T(27), DEN(28), VIS(29), TE(31), ED(32), enthalpy(57) -// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! -// Variables order must from small to big. -// plotFieldType: If dump out the field results to visulization. - -int plotFieldType = 1; -int nVisualVariables = 4; -int visualVariables[] = [22, 23, 24, 25]; - -######################################################################### -# Flow Parameter # -######################################################################### -string FLOW[] = "FLOW"; - -// Initial value of variables or constant -double initRho = 998.3; -double initMu = 1.93345725; -double initU = 0.1; -double initV = 0; -double initW = 0; -double initP = 0; - -// Relaxing factor -double urfU = 0.4; -double urfV = 0.4; -double urfW = 0.4; -double urfP = 0.3; -double urfFlux = 0.4; - -// Tolerance for governing equations -double resU = 1e-6; -double resV = 1e-6; -double resW = 1e-5; -double resP = 1e-5; - -// Solver for solving linear system -// : CGS/GMRES/BiCGSTAB/AMG -string iterSolvU = "BiCGSTAB"; -string iterSolvV = "BiCGSTAB"; -string iterSolvW = "BiCGSTAB"; -string iterSolvP = "GMRES"; - -// Max Iter for solving linear system -int maxSweepU = 30; -int maxSweepV = 30; -int maxSweepW = 30; -int maxSweepP = 30; - -// Tolerance for solving linear system -double iterSolvTolU = 1e-4; -double iterSolvTolV = 1e-4; -double iterSolvTolW = 1e-4; -double iterSolvTolP = 1e-3; - -// Gradient Calculation -// : GAUSS/LSQ -string UGradCalc = "GAUSS"; -string VGradCalc = "GAUSS"; -string WGradCalc = "GAUSS"; -string PGradCalc = "GAUSS"; - -// Convection scheme -// : UPWIND/CDS/QUICK/SUDS -string flowConvCalc = "QUICK"; - -// Diffusion scheme(central difference) -// : NON_ORTHOGONAL -string flowDiffCalc = "NON_ORTHOGONAL"; - -// Transient scheme -// : CRANK_NICOLSON/IMPLICIT_2ND_ORDER/IMPLICIT_EULER -string flowTranCalc = "IMPLICIT_EULER"; - -// Source for flow -// : FLOW_DEFAULT/FLOW_GRAVITY -string flowSourceCalc[] = "FLOW_DEFAULT"; - -//string flowSourceCalc[] = "FLOW_DEFAULT FLOW_GRAVITY"; -int bodyForceFlag = 0; -//double gravityX = 0.0; -//double gravityY = -9.81; -//double gravityZ = 0.0; - -######################################################################### -# Turbulence Parameter # -######################################################################### -//int viscousType = 13; //SPALART_ALLMARAS = 11, KEPSILON = 13 - -//turb SA -//string TURB_SA[] = ["TURB_SA"]; -//string TURB_SA_SCALAR_NAME[] = ["kinetic"]; -//double urfMu = 1.0; - -//double kineticInitValue = 1.0; -//string kineticConvCalc = "UPWIND"; -//string kineticDiffCalc = "NON_ORTHOGONAL"; -//string kineticSourceCalc[] = "TURB_SA_DEFAULT"; -//double kineticUrf = 1.0 -//double kineticRes = 1e-6; - -//string turbIterSolv = "BiCGSTAB"; -//int turbMaxSweep = 30; -//double turbIterSolvTol = 1e-12; - - -//turb K-EPSILON -string TURB_K_EPSILON[] = ["TURB_K","TURB_EPSILON"]; -string TURB_K_EPSILON_SCALAR_NAME[] = ["kinetic", "epsilon"]; - -string TURB_K[] = ["TURB_K"]; -string TURB_K_SCALAR_NAME[] = ["kinetic"]; -string TURB_EPSILON[] = ["TURB_EPSILON"]; -string TURB_EPSILON_SCALAR_NAME[] = ["epsilon"]; -double urfMu = 0.4; - -// turb k -double kineticInitValue = 3.750003e-05; -string kineticConvCalc = "UPWIND"; -string kineticDiffCalc = "NON_ORTHOGONAL"; -string kineticSourceCalc[] = "TURB_K_DEFAULT"; -double kineticUrf = 0.4; -double kineticRes = 1e-6; - -// turb epsilon -double epsilonInitValue = 8.664311e-07; -string epsilonConvCalc = "UPWIND"; -string epsilonDiffCalc = "NON_ORTHOGONAL"; -string epsilonSourceCalc[] = "TURB_EPSILON_DEFAULT"; -double epsilonUrf = 0.4; -double epsilonRes = 1e-6; - -######################################################################### -# Energy Parameter # -######################################################################### -// energyType: The energy solver switch. 0-off, 1-on -// ENERGY[]: Solver binding for factory mode. -// ENERGY_SCALAR_NAME[]: The name of variable to be solved in energy equation. -// energyPrintName[]: The output on the screen during the solution. -int energyType = 0; -string ENERGY[] = ["ENERGY"]; -string ENERGY_SCALAR_NAME[] = "enthalpy"; -string energyPrintName[] = ["H"]; - -// Initial value of variables or constant -double initT = 273.0; -double initK = 0.026; -double initCPg = 1007.0; -double urfT = 0.8; -double urfH = 0.7; -double enthalpyInitValue = 0.21; - -// Discrete schemes -string energyConvCalc = "UPWIND"; -string energyDiffCalc = "NON_ORTHOGONAL"; -string energySourceCalc[] = ["EMPTY"]; -string energyGradCalc = "GAUSS"; -string energyTranCalc = "IMPLICIT_EULER"; - -// Set for solving linear equations -string enthalpyIterSolv = "BiCGSTAB"; -int enthalpyMaxSweep = 30; -double enthalpyIterSolvTol = 1e-12; -double enthalpyRes = 1e-6; \ No newline at end of file diff --git a/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/grid_para.hypara b/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/grid_para.hypara deleted file mode 100644 index 43b3aa9..0000000 --- a/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/grid_para.hypara +++ /dev/null @@ -1,30 +0,0 @@ -######################################################################### -# Grid data type # -######################################################################### -// gridtype: Grid type for generation, conversion, reconstruction, merging. -// 0 -- Unstructured grid. -// 1 -- Structured grid. -// axisup: Type of Cartisien coordinates system, used in grid conversion. -// 1 -- Y upward. (default) -// 2 -- Z upward. -// from_gtype: Type of grid data type in grid conversion process. -// -1 -- MULTI_TYPE. -// 1 -- PHengLEI, *.fts. -// 2 -- CGNS, *.cgns. -// 3 -- Plot3D type of structured grid, *.dat/*.grd. -// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. -// 5 -- Fluent, *.cas/*.msh. -// 6 -- Ustar, mgrid.in. -// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. -// 8 -- GMSH, *.msh. -int gridtype = 0; -int axisup = 1; -int from_gtype = 5; - -######################################################################### -# File path # -######################################################################### -// from_gfile: path of original data file for unstructure grid convert from. -// out_gfile: path of target file for grid convert to, *.fts type of file usually. -string from_gfile = "./grid/suboff.cas"; -string out_gfile = "./grid/suboff.fts"; diff --git a/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/grid/网格地址.txt b/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/grid/网格地址.txt deleted file mode 100644 index 899f977..0000000 --- a/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/grid/网格地址.txt +++ /dev/null @@ -1,5 +0,0 @@ -红山开源风雷算例库原始网格获取百度网盘链接： -链接：http://pan.baidu.com/s/1aZ9cdkp6CkT9il4fEpnTcA -提取码：w47m - -注：plot3D格式网格需同时下载.grd和.inp文件 \ No newline at end of file diff --git a/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/cfd_para.hypara b/L01_TwoD_Cavity_BGK_MPI_1CPU/bin/cfd_para.hypara similarity index 60% rename from H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/cfd_para.hypara rename to L01_TwoD_Cavity_BGK_MPI_1CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/cfd_para.hypara +++ b/L01_TwoD_Cavity_BGK_MPI_1CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # Default parameters for Grid conversion # ########################################################################### // gridtype: Grid type for generation, conversion, reconstruction, merging. -// 0 -- Unstructured grid. -// 1 -- Structured grid. -// 2 -- Hybrid grid, include both of unstructured and structured grid. -// gridobj: Task type of grid treatment. -// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc. -// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS. -// 2 -- Grid refinement. -// 3 -- Grid merging, merge two blocks into one block. -// 4 -- Grid deformation, achieve unstructured grid deformation. -// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells. -// 6 -- Grid mirroring, mirror a symmetry grid to whole grid. -// 7 -- Grid type change, convert structured grid to unstructured grid. +// 0 -- Unstructured grid. +// 1 -- Structured grid. +// 2 -- Hybrid grid, include both of unstructured and structured grid. +// gridobj: Task type of grid treatment. +// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc. +// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS. +// 2 -- Grid refinement. +// 3 -- Grid merging, merge two blocks into one block. +// 4 -- Grid deformation, achieve unstructured grid deformation. +// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells. +// 6 -- Grid mirroring, mirror a symmetry grid to whole grid. +// 7 -- Grid type change, convert structured grid to unstructured grid. // multiblock: Multi-block grid or not, only for structured grid conversion. // 0 -- Not. // 1 -- Yes. @@ -46,19 +47,24 @@ int gridobj = 1; int multiblock = 0; int iadapt = 0; int SymmetryFaceVector = 1; - int gridReorder = 0; int faceReorderMethod = 0; -// axisup: Type of Cartisien coordinates system, used in grid conversion. -// 1 -- Y upward. (default) -// 2 -- Z upward. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". // 0 -- Interface. (default) // 1 -- Physical boundary condition, used in Hybrid solver. int omit_no_bound_bc = 0; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ int dumpOldGrid = 0; // from_gfile: path of original data file for unstructure grid convert from. // out_gfile: path of target file for grid convert to, *.fts type of file usually. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ int fileformat = 0; // Parameters for hybrid solver. // mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type. -// mixgrid_str: path of structure grid file for hybrid solver, *.fts type. -string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; -string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; +// mixgrid_str: path of structure grid file for hybrid solver, *.fts type. +string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; +string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; // Some parameters for structured overlapping grid. int codeOfDigHoles = 1; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 2 -- refine structured grid. // maxproc: The number of partition zones that want to be divided into. // numberOfMultifile: The number of partition grid files that want to be dumped out. - int pgridtype = 0; int maxproc = 4; int numberOfMultifile = 1; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 0 -- Not. // 1 -- Yes. // blockIndexOfMark: the block index of mark, only for structured grid partition. -// cellIndexOfMark: the cell index of mark, only for structured grid partition. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +int cellIndexOfMark[] = [185, 30, 1]; -// parallel Strategy: -//! -# 0 : each zone is assigned to the one that defined in grid partition procedure. -//! -# 1 : random assigned for each zone or by some else ways. -int parallelStrategy = 1; +// parallelStrategy: +// 0 -- each zone is assigned to the one that defined in grid partition procedure. +// 1 -- random assigned for each zone or by some else ways. +int parallelStrategy = 1; //----------------------------------------------------------------------- # File path # //----------------------------------------------------------------------- -// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). +// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). // partition_grid_file: Target partition grid file(PHengLEI type, *.fts). string original_grid_file = "./grid/sphere_mixed.fts"; string partition_grid_file = "./grid/sphere_mixed__4.fts"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 1 -- perfect balance. // maxproc -- perfect imbalance. // 1.05 -- recommended. - int omit_no_bound_bc = 0; int npartmethod = 1; int parallelPartitionMethod = 2; -double parmetisBalance = 1.05; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ int numberOfMultigrid = 1; # Default parameters for CFD simulation # ######################################################################### // maxSimuStep: The max simulation step, don't care simulation is restart or not. -// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. -// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. +// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. +// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved. -// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. -// intervalStepRes: The step intervals for residual file 'res.dat' saved. -// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. -// 0 -- no precondition process. (default, mach > 0.3) -// 1 -- carry out precondition process. (mach number <= 0.3) - -int maxSimuStep = 20000; - -int intervalStepFlow = 1000; -int intervalStepPlot = 1000; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. +// 0 -- no precondition process. (default, mach > 0.3) +// 1 -- carry out precondition process. (mach number <= 0.3) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // freestream_vibration_temperature: Dimensional freestream vibration temperature. // refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition. // height: Fly height, unit of km. // wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition. -// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like: -// 1 dm = 0.1 m. -// 1 cm = 0.01 m. -// 1 mm = 0.001m. -// 1 inch = 0.0254m. -// 1 foot = 12 inches = 0.3048m. -// 1 yard = 3 feet = 0.9144m. +// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter. Common dimensions like: +// 1 dm = 0.1 m. +// 1 cm = 0.01 m. +// 1 mm = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit. // TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit. // radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary // condition is radiation equilibrium temperature, and 0.8 is the default value. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// refMolecularWeight: the reference molecular weight of gas used for perfect gas. The unit is g/mol. // Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on. - -int directionMethod = 0; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2). //double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)). -//int inflowParaType = 3; -//int nsubsonicInlet = 1; -//int nsubsonicOutlet = 1; -//string inLetFileName = "./bin/subsonicInlet.hypara"; -//string outLetFileName = "./bin/subsonicOutlet.hypara"; -//double refDimensionalTemperature = 288.144; -//double refDimensionalPressure = 1.01313E05; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ double forceReferenceArea = 1.0; // unit of meter^2. double TorqueRefX = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# Struct Solver * +#************************************************************************ // inviscidSchemeName: Spatial discretisation scheme of struct grid. // Using this when solve structered grid or hybrid. -// -- "vanleer", "steger", "hlle", "lax_f". -// -- "roe", "modified_roe". +// -- "vanleer", "steger", "hlle", "lax_f", +// -- "roe", "modified_roe", // -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+". // isWennScheme: If using WENN Scheme of struct grid. -// 0 -- NO. (default) -// 1 -- Yes. +// 0 -- NO. (default) +// 1 -- Yes. // str_limiter_name: Limiter of struct grid. -// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth". -// -- "nolim", no limiter. -// -- "vanalbada_clz", clz supersonic version. -// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3" - +// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth", +// -- "nolim", no limiter, +// -- "vanalbada_clz", clz supersonic version, +// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3". string inviscidSchemeName = "roe"; int isWennScheme = 0; -string str_limiter_name = "vanalbada"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 3 -- IDDES. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // Using this when solve Unstructered grid or hybrid. -// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "barth", "vencat", "vanleer", "minmod", +// -- "vanalbada", "smooth", "nnd", "lpz", "1st", // -- "nolim", no limiter. // uns_vis_name: Discretisation method of viscous term. // -- "std", "test", "aver", "new1", "new2". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "default", "ggcell", "ggnode", "lsq". // ivencat: Variation of vencat limiter. // 0 -- org method, it is independent of grid scale. // 1 -- new method, it is dependent of grid scale. @@ -442,18 +451,18 @@ string str_limiter_name = "vanalbada"; // 3 -- Harten type, which is default used. // roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0. // It is used to scale the default Roe entropy fix coefficients. -// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 1.0; // statisticalTimePeriod: Used as time period of statistic analysis. // when the value is negative, time period is treated as infinite. // statisticMethod: Statistic reynolds stress method. -// 0 -- tau = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // min_sub_iter: The min sub iteration of unsteady simulation. // max_sub_iter: The max sub iteration of unsteady simulation. // tol_sub_iter: The tolerance of sub iteration of unsteady simulation. // tscheme: Temporal Discretisation method. -// 1 -- Runge-Kutta Multi-State. -// 2 -- Point implicit. -// 3 -- Full implicit. -// 4 -- LU-SGS. -// 5 -- Block LU-SGS. -// 6 -- Jacobian iteration. -// 7 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // CFLStart: Started cfl number. // CFLEnd: End cfl number. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS. // ifLocalTimeStep: Time step method. -// 0 --Local. -// 1 --Global. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 0 -- global unified CFL number. +// 1 -- local CFL number. // isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no. // visl_min: Minimum value of laminar viscosity coefficient. // turbCFLScale: Turbulence model cfl number factor. // codeOfAleModel: Arbitrary Lagrangian-Eulerian method. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 0 -- no ALE method. +// 1 -- ALE method for non-moving grids. +// 2 -- ALE method for moving grids. +// 3 -- ALE method for deforming grids. // wallFunctionType: The type of wall function to implement. -// 0 -- no wall function. (default) -// 1 -- standard wall function. -// 2 -- Pab3D wall function. +// 0 -- no wall function. (default) +// 1 -- standard wall function. +// 2 -- Pab3D wall function. // RKStage: The number of Runge-Kutta step. // lamda: Cofficient of Runge-Kutta step. - -int iunsteady = 0; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2. int methodOfDualTime = 3; int min_sub_iter = 50; int max_sub_iter = 50; double tol_sub_iter = 0.01; -int tscheme = 4; +int tscheme = 4; int iSimplifyViscousTerm = 1; int ifLocalTimeStep = 0; int isUseLocalCFL = 0; int isUsePreTwall = 0; -double CFLStart = 0.01; -double CFLEnd = 10.0; -int CFLVaryStep = 500; - +double CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# File In or Out * +#************************************************************************ // numberOfGridGroups: The number of grid groups. // gridfile: The partitioned Grid file path, using relative path, // which is relative to the working directory. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps. // restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps. // turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps. -// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps. +// visualfile: The visualization file path of flowfield, write data for every default (intervalStepPlot) steps. // wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps. // nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. // nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. // nIsComputeWallDist: Whether to compute the wall distance. // 0 -- Compute wall distance. // 1 -- Not compute. -// -// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism. -// wall_heatfluxfile : The file to output the MaxHeatFlux of wall. - -int numberOfGridGroups = 1; -string gridfile = "./grid/rae2822_hybrid2d__4.fts"; -string wallTemperaturefile= ""; +// protectionFile0 and protectionFile1: Two continuation file of the data protection mechanism. +// wall_heatfluxfile: The file to output the MaxHeatFlux of wall. +int numberOfGridGroups = 1; +string gridfile = "./grid/rae2822_hybrid2d__4.fts"; +string wallTemperaturefile = ""; int nIsComputeWallDist = 0; int walldistMethod = 1; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), -// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52), -// -- overlap iblank(iblank, 81) - -// -- specific heat ratio(gama, 56) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11), -// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15) -// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19) -// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- heat flux of species diffusion term(Qs, 9), heat flux of vibrational temperature term(Qv, 10), heat flux of electron temperature term(Qe, 11), +// -- species mass fractions(Ns, 12), x component of wall velocity(Vx, 13), y component of wall velocity(Vy, 14), z component of wall velocity(Vz, 15), +// -- slip translational-rotational temperature(Tts, 16), slip vibrational temperature(Tvs, 17), slip electron temperature(Tes, 18), absolute wall velocity(Vs, 19), +// -- Stanton number(St, 20), coefficient of heat rate(Ch, 21), temperature jump(deltaT, 22), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ int dumpStandardModel = 0; // 1 -- Real cell where the probe is located. // nProbeVariables: Number of variables want to be dumped for probes monitered. // probeVariables : Variable types dumped, listed as following: -// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!! // probeVariables order must from small to big. // probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables. -// 0 -- Take the value of probe's cell as probe real value. -// 1 -- Interpolation from probe's and neighbouring cell to probe. -// 2 -- Interpolation from probe's cell nodes to probe. +// 0 -- Take the value of probe's cell as probe real value. +// 1 -- Interpolation from probe's and neighbouring cell to probe. +// 2 -- Interpolation from probe's cell nodes to probe. int ifSetDataMonitor = 0; -int dataMonitorType = 0; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// transitionType: transition model type // 0 -- none. // 2 -- gama-re-theta. -// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition -// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not - - +// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition. +// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not. int turbInterval = 1; int turbOrderStruct = 2; int kindOfTurbSource = 0; int mod_turb_res = 0; -double turb_relax = 1.0; double freeStreamViscosity = 1.0e-3; double muoo = 3.0; double kwoo = 5.0; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - not. +// = 1 -- Create LESSolver; +// != 1 -- not. // amplitudeofDisturb: Amplitude of adding disturb. // disturbstep: Unsteady time step or steady iteration of adding random disturb. // iterdisturb: Add random disturb in every sub-iter or only first sub-iter. -// = 0 - in only first sub-iter; -// != 0 - in every sub-iter. +// = 0 -- in only first sub-iter; +// != 0 -- in every sub-iter. // ipraddisturb: Add density and pressure disturb or not. // ibodyforce: Add body force in source flux of NS equations or not. -// = 0 - not; -// != 0 - Add body force. +// = 0 -- not; +// != 0 -- Add body force. // bodyforce: Body force in source flux of NS equations or not. // utau: friction velocity, using in DNSDisturb. // sgsmodel: subgrid scale model. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak); -// = 2 - pow(deltai * deltaj *deltak, 1/3); -// = 3 - Devloped by Scotti. -// wallDampingFunctionType: = 0 - no wall function; -// = 1 - van Driest; -// = 2 - developed by Dr. Deng Xiaobing; -// = 3 - developed by Piomelli. +// deltaFunctionType: = 1 -- MAX(deltai, deltaj, deltak); +// = 2 -- pow(deltai * deltaj *deltak, 1/3); +// = 3 -- Devloped by Scotti. +// wallDampingFunctionType: = 0 -- no wall function; +// = 1 -- van Driest; +// = 2 -- developed by Dr. Deng Xiaobing; +// = 3 -- developed by Piomelli. // turbViscousCutType: turbulent viscosity cut type. -// = 0 - mu_total = mut + mul; -// = 1 - mu_total = max(mut-mul,0)+ mul; -// = 2 - mu_total = max(mut ,0)+ mul. +// = 0 -- mu_total = mut + mul; +// = 1 -- mu_total = max(mut-mul, 0) + mul; +// = 2 -- mu_total = max(mut , 0) + mul. // smagConstant: constant of smagorinsky model. // waleConstant: constant of wale model. -// filterDirection[3]: filter variables in i, j, k direction or not. +// filterDirection [3]: filter variables in i, j, k direction or not. // averageDirection[3]: average variables in i, j, k direction or not. // isotropicConstant: constant of isotropic part of SGS stress. - int iLES = 0; string sgsmodel = "smagorinsky"; int deltaFunctionType = 2; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# Other Parameters for Hypersonic Non-equilibrium Gas * +#************************************************************************ // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: // 0 -- gas model is fixed in the codes. // 1 -- gas model is imported from library files. -// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver, -// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver. -// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps. -// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // nIdealState: whether take all gas species as ideal gas for gas-mixture process. // 0 -- No. -// 1 -- Yes. -// nTEnergyModel: the method to computing temperature energy model. +// 1 -- Yes. // nTEnergyModel: the method to computing temperature energy model. // 0 -- the energy term is computed using the conventional method. // 1 -- the energy term is computed using the polynomial fitting method. // 2 -- the energy term is computed using the piecewise polynomial fitting method. // parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model. // The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value. // catalyticCoef: -// 0.0 -- full non-catalytic wall boundary condition. -// 1.0 -- full catalytic wall boundary condition. -// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// nTemperatureJump : the method to calculate the temperature jump. -// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode. -// 1 -- the general method where the iteration is calculated with the translation-rotation temperature. -// nSurfGradMethod : the method to compute the surface heating ratio. -// 0 -- the gradient of variable is computed with the first-order difference method. -// 1 -- the gradient of variable is computed with the Green-Guass integral method. -// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero. -// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes. -// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value. -// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping. +// 0.0 -- full non-catalytic wall boundary condition. +// 1.0 -- full catalytic wall boundary condition. +// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// nTemperatureJump: the method to calculate the temperature jump. +// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode. +// 1 -- the general method where the iteration is calculated with the translation-rotation temperature. +// nSurfGradMethod: the method to compute the surface heating ratio. +// 0 -- the gradient of variable is computed with the first-order difference method. +// 1 -- the gradient of variable is computed with the Green-Guass integral method. +// nRapidFlowfield: initialize the flowfield using the rapid engineering method when it is greater than zero. +// nSurfHeatMonitor: To exam the surface heating change or not. 0 is no, 1 is yes. +// nInitPressureStep: the steps to initialize the boundary variables when the rapid method is used. 100 is the default value. +// nDumpCFLNumber: 1 indicates dumping the CFL number to file, 0 denotes no dumping. // sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0]. // sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0]. // sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// spectrumRadiusCoef: The value is in range of [0.0, 2.0]. -// staticPressureRelaxCorf: The value is in range of [0.1, 1.0]. -// nIsChemicalFreeze : the flag to freeze the chemical reactions. -// 0 -- not freeze, the chemical reaction sources will be calculated. -// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te - -//maxViscous: the maximum of Viscous. -//trTemperatureMin: the minimum value of trTemperature. -//veTemperatureMin: the minimum value of veTemperature. -//densityMin: the minimum value of density. -//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0]. -// nDebug: cout the Wrong place and abort -// 0 -- not used. -// 1 -- used. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// spectrumRadiusCoef: The value is in range of [0.0, 2.0]. +// staticPressureRelaxCorf: The value is in range of [0.1, 1.0]. +// nIsChemicalFreeze: the flag to freeze the chemical reactions. +// 0 -- not freeze, the chemical reaction sources will be calculated. +// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated. +// veTemperatureMin: The minimum of Tv and Te. +// maxViscous: the maximum of Viscous. +// trTemperatureMin: the minimum value of trTemperature. +// veTemperatureMin: the minimum value of veTemperature. +// densityMin: the minimum value of density. +// tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0]. +// nDebug: cout the Wrong place and abort +// 0 -- not used. +// 1 -- used. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid -// 0 -- not used. -// 1 -- used. -// nViscosityPeModified: Pe Modified for ViscosityCoef -// 0 -- not used. -// 1 -- used. -// nChemcalSourceModified: Modified on ChemcalSource -// 0 -- not used. -// 1 -- used. -// nChemcalSourceEsMethod: Modified on ChemcalSource -// 0 -- approximation algorithm 1 (Ori.) -// 1 -- approximation algorithm 2 (New) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid. +// 0 -- not used. +// 1 -- used. +// nViscosityPeModified: Pe Modified for ViscosityCoef. +// 0 -- not used. +// 1 -- used. +// nChemcalSourceModified: Modified on ChemcalSource. +// 0 -- not used. +// 1 -- used. +// nChemcalSourceEsMethod: Modified on ChemcalSource. +// 0 -- approximation algorithm 1 (Ori). +// 1 -- approximation algorithm 2 (New). // nMaxStepTemperature: the iterative steps of temperature. - -// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs -// 0 -- not used -// 1 -- used - -// nDiagonalModified: Modified on Diagonal -// 0 -- not used -// 1 -- Ori. -// 2 -- new - -//nGradPrimtiveMethod: -// 0 -- Ori. -// 1 -- new +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 0 -- Blottner fitting method(N89). +// 1 -- Gupta fitting method(N90). // nContinueModel: The new continue model can switch different computation model. -// 0 -- Not use the new continue model. -// 1 -- use the new continue model. +// 0 -- Not use the new continue model. +// 1 -- use the new continue model. // nSutherland: -// 0 -- stands for selecting the Blotter curve fits mode. -// 1 -- stands for Sutherland relation. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11". -// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. -// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. -// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. -// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 NO CO CO2 H2 N2 Air CH4. -// For self-definition model, the gasfile is used to indicate the file path of the new gas model. +// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. +// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. +// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "Gas-Mixture" -- indicates the process of mixing gas without reacting. +// for struct solver mixing two species��SpeciesA, SpeciesB��. +// for unstruct solver mixing multi-species��O2 NO CO CO2 H2 N2 Air CH4��. +// For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. // ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes. -// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation. -// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation. -// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation. -// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory. -// 0 -- no, -// 1 -- yes. +// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation. +// nIterSecondStep: the maximum number of iteration in the second step for the self-adaptive calculation. +// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation. +// nEnergyAssembly: the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory. +// 0 -- no, +// 1 -- yes. // nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model. -// 0 -- the density. -// 1 -- the translation temperature. -// 2 -- the vibration temperature. -// 3 -- the electron temperature. -// 4 -- the pressure. -// 5 -- the mass fraction of oxygen. -// 6 -- the mass fraction of nitrogen. +// 0 -- the density. +// 1 -- the translation temperature. +// 2 -- the vibration temperature. +// 3 -- the electron temperature. +// 4 -- the pressure. +// 5 -- the mass fraction of oxygen. +// 6 -- the mass fraction of nitrogen. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. -// useHyflowSetting : Setting for HyFLOW GUI. -// 0 -- PHengLEI -// 1 -- HyFLOW -// nProtectData : Use the continuation file data protection mechanism. -// 0 -- no -// 1 -- yes - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +double refGama = 1.4; +double prl = 0.72; +double prt = 0.90; +double sc_l = 0.5; +double sc_t = 0.5; -int nGasModel = 0; -int nchem = 0; -int nchemsrc = 1; -int nchemrad = 1; -int ntmodel = 1; +int nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 0; -int nDebug = 0; -int nSpeciesLimit = 1; -int nTurblenceForChemical = 0; -int nViscosityFluxSublevelModified = 1; -int nViscosityPeModified = 0; -int nChemcalSourceModified = 2; -int nChemcalSourceEsMethod = 1; -int nMaxStepTemperature = 5; -int veTemperatureMinModified = 1; -int nDiagonalModified = 0; -int nGradPrimtiveMethod = 1; -int nInviscidFluxModify = 1; -int nQlLimitMethod = 2; -int nSpeciesForWallMethod = 1; -int nDensityForWallMethod = 0; +int nDebug = 0; +int nSpeciesLimit = 1; +int nTurblenceForChemical = 0; +int nViscosityFluxSublevelModified = 1; +int nViscosityPeModified = 0; +int nChemcalSourceModified = 2; +int nChemcalSourceEsMethod = 1; +int nMaxStepTemperature = 5; +int veTemperatureMinModified = 1; +int nDiagonalModified = 0; +int nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; //string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; //string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; -//string gasfile = "Pa"; +//string gasfile = "Pa"; //string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ int ismooth_turb = 0; int SAProductType = 2; // ----------------- Overset Grid parameter ----------------------------- -int codeOfDigHoles = 1; -int codeOfTurbulentModel = 0; -string masterFileName = "./grid/searchFile.inp"; -string holeBasicFileName = "./grid/holeBasicFile.inp"; -string holeFullFileName = "./grid/holeFullFile.dat"; -string linkFileName = "./grid/topology.dat"; -string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; +int codeOfDigHoles = 1; +int codeOfTurbulentModel = 0; +string masterFileName = "./grid/searchFile.inp"; +string holeBasicFileName = "./grid/holeBasicFile.inp"; +string holeFullFileName = "./grid/holeFullFile.dat"; +string linkFileName = "./grid/topology.dat"; +string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; -######################################################################### -# High Order Struct Solver # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 0 -- NSSolverStruct using Finite Volume Method. +// 1 -- NSSolverStruct using Finite Differ Method. // SolverStructOrder: Spatial discretisation order of NS equations with struct grid. // <= 2 -- finite volume method. // >= 3 -- finite difference order. (to be completed) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.ovs"; -double walldistMainZone = 1.0 -double toleranceForOversetSearch = 1.0e-3; -double toleranceForOversetBox = 1.0e-3; -int twoOrderInterpolationOrNot = 0; -int keyEnlargeOfActiveNodes = 0; -int outTecplotOverset = 0; -int outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.ovs"; +double walldistMainZone = 1.0 +double toleranceForOversetSearch = 1.0e-3; +double toleranceForOversetBox = 1.0e-3; +int twoOrderInterpolationOrNot = 0; +int keyEnlargeOfActiveNodes = 0; +int outTecplotOverset = 0; +int outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ double referenceLength = 1.0; double referenceVelocity = 1.0; double referenceDensity = 1.0; -int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd; -int strategyForGCLSource = 0; //0-present; 1-Ahn; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +int RBDMethod_0 = 0; +double amplitude_0 = 0.0; +double reduceFrequency_0 = 0.0; +// direction of rotation. // 1 -- clockwise from the point of view along the positive x axis. // -1 -- anticlockwise from the point of view along the positive x axis. -int direction_0 = -1; -double rotateFrequency_0 = 0.0; -//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; -//additional force (system axis) fX fY fZ -double addedForce_0[] = 0.0 ,0.0 ,0.0 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/L01_TwoD_Cavity_BGK_MPI_1CPU/bin/input.txt b/L01_TwoD_Cavity_BGK_MPI_1CPU/bin/input.txt new file mode 100644 index 0000000..c49c94a --- /dev/null +++ b/L01_TwoD_Cavity_BGK_MPI_1CPU/bin/input.txt @@ -0,0 +1,35 @@ +0 ！MRT set 1, BGK set 0 +0 continue.plt ！CONTI, resume :1 , new 0 //follows input datafile name //use ASCII文件 continue.plt +0 ！LES yes: 1 , no: 0 +0 mesh_3d.dat ！GEO read complex geo? yes:1, no:0 //follows input datafile name +0 ! MB multiblock LBM? yes:1, no:0 +1 2e-3 !CONV using converge criterion? yes:1, no:0 +201 ！NX +201 ! NY +1 ! NZ +1 ！ NX2 +1 ！ NY2 +1 ! NZ2 +0 ! LowX +0 ! LowY +0 ! LowZ +1 ! x_np +1 ! y_np +1 ! z_np +500 ! framerate +50000 ！total steps to terminate +1.0 ! density +0.6 ！ tau +(0.0, 0.0, 0.0000000) ！ Volumetric force vector (gx, gy, gz) +D2Q9 ! velocity set +Cavity ! boundary condition +! note: in the following, boundary types: periodic,velocity, pressure +! are allowed. if "velocity" is applied, please strictly follow the format "velocity (%lf, %lf, %lf)". +nonslip ！xmin face +nonslip ！xmax face +nonslip ！ymin face +velocity (0.1, 0.0, 0.0) ！ymax face, +periodic ！zmin face +periodic ！zmax face +-------------------！ initial velocity field +(0.0, 0.00, 0.0) \ No newline at end of file diff --git a/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/key.hypara b/L01_TwoD_Cavity_BGK_MPI_1CPU/bin/key.hypara similarity index 91% rename from H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/key.hypara rename to L01_TwoD_Cavity_BGK_MPI_1CPU/bin/key.hypara index 9c32184..98d46f2 100644 --- a/H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU/bin/key.hypara +++ b/L01_TwoD_Cavity_BGK_MPI_1CPU/bin/key.hypara @@ -17,12 +17,12 @@ string defaultParaFile = "./bin/cfd_para.hypara"; int ndim = 2; int nparafile = 1; -int nsimutask = 0; -string parafilename = "./bin/cfd_para_incompressible.hypara" +//int nsimutask = 0; //string parafilename = "./bin/cfd_para_subsonic.hypara"; //string parafilename = "./bin/cfd_para_transonic.hypara"; //string parafilename = "./bin/cfd_para_supersonic.hypara"; //string parafilename = "./bin/cfd_para_hypersonic.hypara"; +//string parafilename = "./bin/cfd_para_incompressible.hypara"; //int nsimutask = 1; //string parafilename = "./bin/grid_para.hypara"; @@ -39,6 +39,9 @@ string parafilename = "./bin/cfd_para_incompressible.hypara" //int nsimutask = 1; //string parafilename = "./bin/grid_refine_para.hypara"; +int nsimutask = 13; +string parafilename = "./bin/cfd_para.hypara"; + //int nsimutask = 14; //string parafilename = "./bin/integrative_solver.hypara"; diff --git a/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/cfd_para.hypara b/L02_ThreeD_Channel_Turb_BGK_MPI_32CPU/bin/cfd_para.hypara similarity index 60% rename from H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/cfd_para.hypara rename to L02_ThreeD_Channel_Turb_BGK_MPI_32CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/cfd_para.hypara +++ b/L02_ThreeD_Channel_Turb_BGK_MPI_32CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # Default parameters for Grid conversion # ########################################################################### // gridtype: Grid type for generation, conversion, reconstruction, merging. -// 0 -- Unstructured grid. -// 1 -- Structured grid. -// 2 -- Hybrid grid, include both of unstructured and structured grid. -// gridobj: Task type of grid treatment. -// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc. -// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS. -// 2 -- Grid refinement. -// 3 -- Grid merging, merge two blocks into one block. -// 4 -- Grid deformation, achieve unstructured grid deformation. -// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells. -// 6 -- Grid mirroring, mirror a symmetry grid to whole grid. -// 7 -- Grid type change, convert structured grid to unstructured grid. +// 0 -- Unstructured grid. +// 1 -- Structured grid. +// 2 -- Hybrid grid, include both of unstructured and structured grid. +// gridobj: Task type of grid treatment. +// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc. +// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS. +// 2 -- Grid refinement. +// 3 -- Grid merging, merge two blocks into one block. +// 4 -- Grid deformation, achieve unstructured grid deformation. +// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells. +// 6 -- Grid mirroring, mirror a symmetry grid to whole grid. +// 7 -- Grid type change, convert structured grid to unstructured grid. // multiblock: Multi-block grid or not, only for structured grid conversion. // 0 -- Not. // 1 -- Yes. @@ -46,19 +47,24 @@ int gridobj = 1; int multiblock = 0; int iadapt = 0; int SymmetryFaceVector = 1; - int gridReorder = 0; int faceReorderMethod = 0; -// axisup: Type of Cartisien coordinates system, used in grid conversion. -// 1 -- Y upward. (default) -// 2 -- Z upward. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". // 0 -- Interface. (default) // 1 -- Physical boundary condition, used in Hybrid solver. int omit_no_bound_bc = 0; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ int dumpOldGrid = 0; // from_gfile: path of original data file for unstructure grid convert from. // out_gfile: path of target file for grid convert to, *.fts type of file usually. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ int fileformat = 0; // Parameters for hybrid solver. // mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type. -// mixgrid_str: path of structure grid file for hybrid solver, *.fts type. -string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; -string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; +// mixgrid_str: path of structure grid file for hybrid solver, *.fts type. +string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; +string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; // Some parameters for structured overlapping grid. int codeOfDigHoles = 1; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 2 -- refine structured grid. // maxproc: The number of partition zones that want to be divided into. // numberOfMultifile: The number of partition grid files that want to be dumped out. - int pgridtype = 0; int maxproc = 4; int numberOfMultifile = 1; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 0 -- Not. // 1 -- Yes. // blockIndexOfMark: the block index of mark, only for structured grid partition. -// cellIndexOfMark: the cell index of mark, only for structured grid partition. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +int cellIndexOfMark[] = [185, 30, 1]; -// parallel Strategy: -//! -# 0 : each zone is assigned to the one that defined in grid partition procedure. -//! -# 1 : random assigned for each zone or by some else ways. -int parallelStrategy = 1; +// parallelStrategy: +// 0 -- each zone is assigned to the one that defined in grid partition procedure. +// 1 -- random assigned for each zone or by some else ways. +int parallelStrategy = 1; //----------------------------------------------------------------------- # File path # //----------------------------------------------------------------------- -// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). +// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). // partition_grid_file: Target partition grid file(PHengLEI type, *.fts). string original_grid_file = "./grid/sphere_mixed.fts"; string partition_grid_file = "./grid/sphere_mixed__4.fts"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 1 -- perfect balance. // maxproc -- perfect imbalance. // 1.05 -- recommended. - int omit_no_bound_bc = 0; int npartmethod = 1; int parallelPartitionMethod = 2; -double parmetisBalance = 1.05; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ int numberOfMultigrid = 1; # Default parameters for CFD simulation # ######################################################################### // maxSimuStep: The max simulation step, don't care simulation is restart or not. -// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. -// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. +// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. +// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved. -// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. -// intervalStepRes: The step intervals for residual file 'res.dat' saved. -// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. -// 0 -- no precondition process. (default, mach > 0.3) -// 1 -- carry out precondition process. (mach number <= 0.3) - -int maxSimuStep = 20000; - -int intervalStepFlow = 1000; -int intervalStepPlot = 1000; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. +// 0 -- no precondition process. (default, mach > 0.3) +// 1 -- carry out precondition process. (mach number <= 0.3) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // freestream_vibration_temperature: Dimensional freestream vibration temperature. // refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition. // height: Fly height, unit of km. // wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition. -// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like: -// 1 dm = 0.1 m. -// 1 cm = 0.01 m. -// 1 mm = 0.001m. -// 1 inch = 0.0254m. -// 1 foot = 12 inches = 0.3048m. -// 1 yard = 3 feet = 0.9144m. +// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter. Common dimensions like: +// 1 dm = 0.1 m. +// 1 cm = 0.01 m. +// 1 mm = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit. // TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit. // radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary // condition is radiation equilibrium temperature, and 0.8 is the default value. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// refMolecularWeight: the reference molecular weight of gas used for perfect gas. The unit is g/mol. // Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on. - -int directionMethod = 0; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2). //double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)). -//int inflowParaType = 3; -//int nsubsonicInlet = 1; -//int nsubsonicOutlet = 1; -//string inLetFileName = "./bin/subsonicInlet.hypara"; -//string outLetFileName = "./bin/subsonicOutlet.hypara"; -//double refDimensionalTemperature = 288.144; -//double refDimensionalPressure = 1.01313E05; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ double forceReferenceArea = 1.0; // unit of meter^2. double TorqueRefX = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# Struct Solver * +#************************************************************************ // inviscidSchemeName: Spatial discretisation scheme of struct grid. // Using this when solve structered grid or hybrid. -// -- "vanleer", "steger", "hlle", "lax_f". -// -- "roe", "modified_roe". +// -- "vanleer", "steger", "hlle", "lax_f", +// -- "roe", "modified_roe", // -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+". // isWennScheme: If using WENN Scheme of struct grid. -// 0 -- NO. (default) -// 1 -- Yes. +// 0 -- NO. (default) +// 1 -- Yes. // str_limiter_name: Limiter of struct grid. -// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth". -// -- "nolim", no limiter. -// -- "vanalbada_clz", clz supersonic version. -// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3" - +// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth", +// -- "nolim", no limiter, +// -- "vanalbada_clz", clz supersonic version, +// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3". string inviscidSchemeName = "roe"; int isWennScheme = 0; -string str_limiter_name = "vanalbada"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 3 -- IDDES. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // Using this when solve Unstructered grid or hybrid. -// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "barth", "vencat", "vanleer", "minmod", +// -- "vanalbada", "smooth", "nnd", "lpz", "1st", // -- "nolim", no limiter. // uns_vis_name: Discretisation method of viscous term. // -- "std", "test", "aver", "new1", "new2". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "default", "ggcell", "ggnode", "lsq". // ivencat: Variation of vencat limiter. // 0 -- org method, it is independent of grid scale. // 1 -- new method, it is dependent of grid scale. @@ -442,18 +451,18 @@ string str_limiter_name = "vanalbada"; // 3 -- Harten type, which is default used. // roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0. // It is used to scale the default Roe entropy fix coefficients. -// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 1.0; // statisticalTimePeriod: Used as time period of statistic analysis. // when the value is negative, time period is treated as infinite. // statisticMethod: Statistic reynolds stress method. -// 0 -- tau = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // min_sub_iter: The min sub iteration of unsteady simulation. // max_sub_iter: The max sub iteration of unsteady simulation. // tol_sub_iter: The tolerance of sub iteration of unsteady simulation. // tscheme: Temporal Discretisation method. -// 1 -- Runge-Kutta Multi-State. -// 2 -- Point implicit. -// 3 -- Full implicit. -// 4 -- LU-SGS. -// 5 -- Block LU-SGS. -// 6 -- Jacobian iteration. -// 7 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // CFLStart: Started cfl number. // CFLEnd: End cfl number. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS. // ifLocalTimeStep: Time step method. -// 0 --Local. -// 1 --Global. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 0 -- global unified CFL number. +// 1 -- local CFL number. // isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no. // visl_min: Minimum value of laminar viscosity coefficient. // turbCFLScale: Turbulence model cfl number factor. // codeOfAleModel: Arbitrary Lagrangian-Eulerian method. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 0 -- no ALE method. +// 1 -- ALE method for non-moving grids. +// 2 -- ALE method for moving grids. +// 3 -- ALE method for deforming grids. // wallFunctionType: The type of wall function to implement. -// 0 -- no wall function. (default) -// 1 -- standard wall function. -// 2 -- Pab3D wall function. +// 0 -- no wall function. (default) +// 1 -- standard wall function. +// 2 -- Pab3D wall function. // RKStage: The number of Runge-Kutta step. // lamda: Cofficient of Runge-Kutta step. - -int iunsteady = 0; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2. int methodOfDualTime = 3; int min_sub_iter = 50; int max_sub_iter = 50; double tol_sub_iter = 0.01; -int tscheme = 4; +int tscheme = 4; int iSimplifyViscousTerm = 1; int ifLocalTimeStep = 0; int isUseLocalCFL = 0; int isUsePreTwall = 0; -double CFLStart = 0.01; -double CFLEnd = 10.0; -int CFLVaryStep = 500; - +double CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# File In or Out * +#************************************************************************ // numberOfGridGroups: The number of grid groups. // gridfile: The partitioned Grid file path, using relative path, // which is relative to the working directory. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps. // restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps. // turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps. -// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps. +// visualfile: The visualization file path of flowfield, write data for every default (intervalStepPlot) steps. // wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps. // nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. // nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. // nIsComputeWallDist: Whether to compute the wall distance. // 0 -- Compute wall distance. // 1 -- Not compute. -// -// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism. -// wall_heatfluxfile : The file to output the MaxHeatFlux of wall. - -int numberOfGridGroups = 1; -string gridfile = "./grid/rae2822_hybrid2d__4.fts"; -string wallTemperaturefile= ""; +// protectionFile0 and protectionFile1: Two continuation file of the data protection mechanism. +// wall_heatfluxfile: The file to output the MaxHeatFlux of wall. +int numberOfGridGroups = 1; +string gridfile = "./grid/rae2822_hybrid2d__4.fts"; +string wallTemperaturefile = ""; int nIsComputeWallDist = 0; int walldistMethod = 1; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), -// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52), -// -- overlap iblank(iblank, 81) - -// -- specific heat ratio(gama, 56) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11), -// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15) -// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19) -// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- heat flux of species diffusion term(Qs, 9), heat flux of vibrational temperature term(Qv, 10), heat flux of electron temperature term(Qe, 11), +// -- species mass fractions(Ns, 12), x component of wall velocity(Vx, 13), y component of wall velocity(Vy, 14), z component of wall velocity(Vz, 15), +// -- slip translational-rotational temperature(Tts, 16), slip vibrational temperature(Tvs, 17), slip electron temperature(Tes, 18), absolute wall velocity(Vs, 19), +// -- Stanton number(St, 20), coefficient of heat rate(Ch, 21), temperature jump(deltaT, 22), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ int dumpStandardModel = 0; // 1 -- Real cell where the probe is located. // nProbeVariables: Number of variables want to be dumped for probes monitered. // probeVariables : Variable types dumped, listed as following: -// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!! // probeVariables order must from small to big. // probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables. -// 0 -- Take the value of probe's cell as probe real value. -// 1 -- Interpolation from probe's and neighbouring cell to probe. -// 2 -- Interpolation from probe's cell nodes to probe. +// 0 -- Take the value of probe's cell as probe real value. +// 1 -- Interpolation from probe's and neighbouring cell to probe. +// 2 -- Interpolation from probe's cell nodes to probe. int ifSetDataMonitor = 0; -int dataMonitorType = 0; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// transitionType: transition model type // 0 -- none. // 2 -- gama-re-theta. -// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition -// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not - - +// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition. +// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not. int turbInterval = 1; int turbOrderStruct = 2; int kindOfTurbSource = 0; int mod_turb_res = 0; -double turb_relax = 1.0; double freeStreamViscosity = 1.0e-3; double muoo = 3.0; double kwoo = 5.0; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - not. +// = 1 -- Create LESSolver; +// != 1 -- not. // amplitudeofDisturb: Amplitude of adding disturb. // disturbstep: Unsteady time step or steady iteration of adding random disturb. // iterdisturb: Add random disturb in every sub-iter or only first sub-iter. -// = 0 - in only first sub-iter; -// != 0 - in every sub-iter. +// = 0 -- in only first sub-iter; +// != 0 -- in every sub-iter. // ipraddisturb: Add density and pressure disturb or not. // ibodyforce: Add body force in source flux of NS equations or not. -// = 0 - not; -// != 0 - Add body force. +// = 0 -- not; +// != 0 -- Add body force. // bodyforce: Body force in source flux of NS equations or not. // utau: friction velocity, using in DNSDisturb. // sgsmodel: subgrid scale model. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak); -// = 2 - pow(deltai * deltaj *deltak, 1/3); -// = 3 - Devloped by Scotti. -// wallDampingFunctionType: = 0 - no wall function; -// = 1 - van Driest; -// = 2 - developed by Dr. Deng Xiaobing; -// = 3 - developed by Piomelli. +// deltaFunctionType: = 1 -- MAX(deltai, deltaj, deltak); +// = 2 -- pow(deltai * deltaj *deltak, 1/3); +// = 3 -- Devloped by Scotti. +// wallDampingFunctionType: = 0 -- no wall function; +// = 1 -- van Driest; +// = 2 -- developed by Dr. Deng Xiaobing; +// = 3 -- developed by Piomelli. // turbViscousCutType: turbulent viscosity cut type. -// = 0 - mu_total = mut + mul; -// = 1 - mu_total = max(mut-mul,0)+ mul; -// = 2 - mu_total = max(mut ,0)+ mul. +// = 0 -- mu_total = mut + mul; +// = 1 -- mu_total = max(mut-mul, 0) + mul; +// = 2 -- mu_total = max(mut , 0) + mul. // smagConstant: constant of smagorinsky model. // waleConstant: constant of wale model. -// filterDirection[3]: filter variables in i, j, k direction or not. +// filterDirection [3]: filter variables in i, j, k direction or not. // averageDirection[3]: average variables in i, j, k direction or not. // isotropicConstant: constant of isotropic part of SGS stress. - int iLES = 0; string sgsmodel = "smagorinsky"; int deltaFunctionType = 2; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# Other Parameters for Hypersonic Non-equilibrium Gas * +#************************************************************************ // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: // 0 -- gas model is fixed in the codes. // 1 -- gas model is imported from library files. -// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver, -// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver. -// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps. -// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // nIdealState: whether take all gas species as ideal gas for gas-mixture process. // 0 -- No. -// 1 -- Yes. -// nTEnergyModel: the method to computing temperature energy model. +// 1 -- Yes. // nTEnergyModel: the method to computing temperature energy model. // 0 -- the energy term is computed using the conventional method. // 1 -- the energy term is computed using the polynomial fitting method. // 2 -- the energy term is computed using the piecewise polynomial fitting method. // parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model. // The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value. // catalyticCoef: -// 0.0 -- full non-catalytic wall boundary condition. -// 1.0 -- full catalytic wall boundary condition. -// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// nTemperatureJump : the method to calculate the temperature jump. -// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode. -// 1 -- the general method where the iteration is calculated with the translation-rotation temperature. -// nSurfGradMethod : the method to compute the surface heating ratio. -// 0 -- the gradient of variable is computed with the first-order difference method. -// 1 -- the gradient of variable is computed with the Green-Guass integral method. -// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero. -// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes. -// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value. -// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping. +// 0.0 -- full non-catalytic wall boundary condition. +// 1.0 -- full catalytic wall boundary condition. +// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// nTemperatureJump: the method to calculate the temperature jump. +// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode. +// 1 -- the general method where the iteration is calculated with the translation-rotation temperature. +// nSurfGradMethod: the method to compute the surface heating ratio. +// 0 -- the gradient of variable is computed with the first-order difference method. +// 1 -- the gradient of variable is computed with the Green-Guass integral method. +// nRapidFlowfield: initialize the flowfield using the rapid engineering method when it is greater than zero. +// nSurfHeatMonitor: To exam the surface heating change or not. 0 is no, 1 is yes. +// nInitPressureStep: the steps to initialize the boundary variables when the rapid method is used. 100 is the default value. +// nDumpCFLNumber: 1 indicates dumping the CFL number to file, 0 denotes no dumping. // sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0]. // sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0]. // sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// spectrumRadiusCoef: The value is in range of [0.0, 2.0]. -// staticPressureRelaxCorf: The value is in range of [0.1, 1.0]. -// nIsChemicalFreeze : the flag to freeze the chemical reactions. -// 0 -- not freeze, the chemical reaction sources will be calculated. -// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te - -//maxViscous: the maximum of Viscous. -//trTemperatureMin: the minimum value of trTemperature. -//veTemperatureMin: the minimum value of veTemperature. -//densityMin: the minimum value of density. -//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0]. -// nDebug: cout the Wrong place and abort -// 0 -- not used. -// 1 -- used. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// spectrumRadiusCoef: The value is in range of [0.0, 2.0]. +// staticPressureRelaxCorf: The value is in range of [0.1, 1.0]. +// nIsChemicalFreeze: the flag to freeze the chemical reactions. +// 0 -- not freeze, the chemical reaction sources will be calculated. +// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated. +// veTemperatureMin: The minimum of Tv and Te. +// maxViscous: the maximum of Viscous. +// trTemperatureMin: the minimum value of trTemperature. +// veTemperatureMin: the minimum value of veTemperature. +// densityMin: the minimum value of density. +// tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0]. +// nDebug: cout the Wrong place and abort +// 0 -- not used. +// 1 -- used. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid -// 0 -- not used. -// 1 -- used. -// nViscosityPeModified: Pe Modified for ViscosityCoef -// 0 -- not used. -// 1 -- used. -// nChemcalSourceModified: Modified on ChemcalSource -// 0 -- not used. -// 1 -- used. -// nChemcalSourceEsMethod: Modified on ChemcalSource -// 0 -- approximation algorithm 1 (Ori.) -// 1 -- approximation algorithm 2 (New) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid. +// 0 -- not used. +// 1 -- used. +// nViscosityPeModified: Pe Modified for ViscosityCoef. +// 0 -- not used. +// 1 -- used. +// nChemcalSourceModified: Modified on ChemcalSource. +// 0 -- not used. +// 1 -- used. +// nChemcalSourceEsMethod: Modified on ChemcalSource. +// 0 -- approximation algorithm 1 (Ori). +// 1 -- approximation algorithm 2 (New). // nMaxStepTemperature: the iterative steps of temperature. - -// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs -// 0 -- not used -// 1 -- used - -// nDiagonalModified: Modified on Diagonal -// 0 -- not used -// 1 -- Ori. -// 2 -- new - -//nGradPrimtiveMethod: -// 0 -- Ori. -// 1 -- new +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 0 -- Blottner fitting method(N89). +// 1 -- Gupta fitting method(N90). // nContinueModel: The new continue model can switch different computation model. -// 0 -- Not use the new continue model. -// 1 -- use the new continue model. +// 0 -- Not use the new continue model. +// 1 -- use the new continue model. // nSutherland: -// 0 -- stands for selecting the Blotter curve fits mode. -// 1 -- stands for Sutherland relation. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11". -// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. -// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. -// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. -// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 NO CO CO2 H2 N2 Air CH4. -// For self-definition model, the gasfile is used to indicate the file path of the new gas model. +// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. +// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. +// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "Gas-Mixture" -- indicates the process of mixing gas without reacting. +// for struct solver mixing two species��SpeciesA, SpeciesB��. +// for unstruct solver mixing multi-species��O2 NO CO CO2 H2 N2 Air CH4��. +// For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. // ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes. -// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation. -// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation. -// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation. -// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory. -// 0 -- no, -// 1 -- yes. +// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation. +// nIterSecondStep: the maximum number of iteration in the second step for the self-adaptive calculation. +// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation. +// nEnergyAssembly: the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory. +// 0 -- no, +// 1 -- yes. // nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model. -// 0 -- the density. -// 1 -- the translation temperature. -// 2 -- the vibration temperature. -// 3 -- the electron temperature. -// 4 -- the pressure. -// 5 -- the mass fraction of oxygen. -// 6 -- the mass fraction of nitrogen. +// 0 -- the density. +// 1 -- the translation temperature. +// 2 -- the vibration temperature. +// 3 -- the electron temperature. +// 4 -- the pressure. +// 5 -- the mass fraction of oxygen. +// 6 -- the mass fraction of nitrogen. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. -// useHyflowSetting : Setting for HyFLOW GUI. -// 0 -- PHengLEI -// 1 -- HyFLOW -// nProtectData : Use the continuation file data protection mechanism. -// 0 -- no -// 1 -- yes - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +double refGama = 1.4; +double prl = 0.72; +double prt = 0.90; +double sc_l = 0.5; +double sc_t = 0.5; -int nGasModel = 0; -int nchem = 0; -int nchemsrc = 1; -int nchemrad = 1; -int ntmodel = 1; +int nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 0; -int nDebug = 0; -int nSpeciesLimit = 1; -int nTurblenceForChemical = 0; -int nViscosityFluxSublevelModified = 1; -int nViscosityPeModified = 0; -int nChemcalSourceModified = 2; -int nChemcalSourceEsMethod = 1; -int nMaxStepTemperature = 5; -int veTemperatureMinModified = 1; -int nDiagonalModified = 0; -int nGradPrimtiveMethod = 1; -int nInviscidFluxModify = 1; -int nQlLimitMethod = 2; -int nSpeciesForWallMethod = 1; -int nDensityForWallMethod = 0; +int nDebug = 0; +int nSpeciesLimit = 1; +int nTurblenceForChemical = 0; +int nViscosityFluxSublevelModified = 1; +int nViscosityPeModified = 0; +int nChemcalSourceModified = 2; +int nChemcalSourceEsMethod = 1; +int nMaxStepTemperature = 5; +int veTemperatureMinModified = 1; +int nDiagonalModified = 0; +int nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; //string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; //string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; -//string gasfile = "Pa"; +//string gasfile = "Pa"; //string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ int ismooth_turb = 0; int SAProductType = 2; // ----------------- Overset Grid parameter ----------------------------- -int codeOfDigHoles = 1; -int codeOfTurbulentModel = 0; -string masterFileName = "./grid/searchFile.inp"; -string holeBasicFileName = "./grid/holeBasicFile.inp"; -string holeFullFileName = "./grid/holeFullFile.dat"; -string linkFileName = "./grid/topology.dat"; -string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; +int codeOfDigHoles = 1; +int codeOfTurbulentModel = 0; +string masterFileName = "./grid/searchFile.inp"; +string holeBasicFileName = "./grid/holeBasicFile.inp"; +string holeFullFileName = "./grid/holeFullFile.dat"; +string linkFileName = "./grid/topology.dat"; +string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; -######################################################################### -# High Order Struct Solver # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 0 -- NSSolverStruct using Finite Volume Method. +// 1 -- NSSolverStruct using Finite Differ Method. // SolverStructOrder: Spatial discretisation order of NS equations with struct grid. // <= 2 -- finite volume method. // >= 3 -- finite difference order. (to be completed) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.ovs"; -double walldistMainZone = 1.0 -double toleranceForOversetSearch = 1.0e-3; -double toleranceForOversetBox = 1.0e-3; -int twoOrderInterpolationOrNot = 0; -int keyEnlargeOfActiveNodes = 0; -int outTecplotOverset = 0; -int outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.ovs"; +double walldistMainZone = 1.0 +double toleranceForOversetSearch = 1.0e-3; +double toleranceForOversetBox = 1.0e-3; +int twoOrderInterpolationOrNot = 0; +int keyEnlargeOfActiveNodes = 0; +int outTecplotOverset = 0; +int outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ double referenceLength = 1.0; double referenceVelocity = 1.0; double referenceDensity = 1.0; -int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd; -int strategyForGCLSource = 0; //0-present; 1-Ahn; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +int RBDMethod_0 = 0; +double amplitude_0 = 0.0; +double reduceFrequency_0 = 0.0; +// direction of rotation. // 1 -- clockwise from the point of view along the positive x axis. // -1 -- anticlockwise from the point of view along the positive x axis. -int direction_0 = -1; -double rotateFrequency_0 = 0.0; -//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; -//additional force (system axis) fX fY fZ -double addedForce_0[] = 0.0 ,0.0 ,0.0 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/L02_ThreeD_Channel_Turb_BGK_MPI_32CPU/bin/input.txt b/L02_ThreeD_Channel_Turb_BGK_MPI_32CPU/bin/input.txt new file mode 100644 index 0000000..4c52feb --- /dev/null +++ b/L02_ThreeD_Channel_Turb_BGK_MPI_32CPU/bin/input.txt @@ -0,0 +1,35 @@ +0 ！MRT set 1, BGK set 0 +1 continue.plt ！CONTI, resume :1 , new 0 //follows input datafile name //use ASCII文件 continue.plt +1 ！LES yes: 1 , no: 0 +0 mesh_3d.dat ！GEO read complex geo? yes:1, no:0 //follows input datafile name +0 ! MB multiblock LBM? yes:1, no:0 +0 2e-3 !CONV using converge criterion? yes:1, no:0 +128 ！NX +128 ! NY +256 ! NZ +1 ！ NX2 +1 ！ NY2 +1 ! NZ2 +0 ! LowX +0 ! LowY +0 ! LowZ +4 ! x_np +4 ! y_np +2 ! z_np +5000 ! framerate +20000 ！total steps to terminate +1.0 ! density +0.506 ！ tau +(9.2e-8,0.0,0.0) ！ Volumetric force +D3Q19 ! velocity set +ChannelTurb ! boundary condition +! note: in the following, boundary types: periodic,velocity, pressure +! are allowed. if "velocity" is applied, please strictly follow the format "velocity (%lf, %lf, %lf)". +periodic ！xmin face +periodic ！xmax face +periodic ！ymin face +periodic ！ymax face, +nonslip ！zmin face +nonslip ！zmax face +-------------------！ initial velocity field +(0.0, 0.00, 0.0) diff --git a/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/key.hypara b/L02_ThreeD_Channel_Turb_BGK_MPI_32CPU/bin/key.hypara similarity index 91% rename from H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/key.hypara rename to L02_ThreeD_Channel_Turb_BGK_MPI_32CPU/bin/key.hypara index 80060fd..1a572c7 100644 --- a/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/key.hypara +++ b/L02_ThreeD_Channel_Turb_BGK_MPI_32CPU/bin/key.hypara @@ -17,12 +17,12 @@ string defaultParaFile = "./bin/cfd_para.hypara"; int ndim = 3; int nparafile = 1; -int nsimutask = 0; -string parafilename = "./bin/cfd_para_incompressible.hypara" +//int nsimutask = 0; //string parafilename = "./bin/cfd_para_subsonic.hypara"; //string parafilename = "./bin/cfd_para_transonic.hypara"; //string parafilename = "./bin/cfd_para_supersonic.hypara"; //string parafilename = "./bin/cfd_para_hypersonic.hypara"; +//string parafilename = "./bin/cfd_para_incompressible.hypara"; //int nsimutask = 1; //string parafilename = "./bin/grid_para.hypara"; @@ -39,6 +39,9 @@ string parafilename = "./bin/cfd_para_incompressible.hypara" //int nsimutask = 1; //string parafilename = "./bin/grid_refine_para.hypara"; +int nsimutask = 13; +string parafilename = "./bin/cfd_para.hypara"; + //int nsimutask = 14; //string parafilename = "./bin/integrative_solver.hypara"; diff --git a/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/cfd_para.hypara b/L03_ThreeD_Poiseuille_MRT_MPI_4CPU/bin/cfd_para.hypara similarity index 60% rename from H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/cfd_para.hypara rename to L03_ThreeD_Poiseuille_MRT_MPI_4CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/cfd_para.hypara +++ b/L03_ThreeD_Poiseuille_MRT_MPI_4CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # Default parameters for Grid conversion # ########################################################################### // gridtype: Grid type for generation, conversion, reconstruction, merging. -// 0 -- Unstructured grid. -// 1 -- Structured grid. -// 2 -- Hybrid grid, include both of unstructured and structured grid. -// gridobj: Task type of grid treatment. -// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc. -// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS. -// 2 -- Grid refinement. -// 3 -- Grid merging, merge two blocks into one block. -// 4 -- Grid deformation, achieve unstructured grid deformation. -// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells. -// 6 -- Grid mirroring, mirror a symmetry grid to whole grid. -// 7 -- Grid type change, convert structured grid to unstructured grid. +// 0 -- Unstructured grid. +// 1 -- Structured grid. +// 2 -- Hybrid grid, include both of unstructured and structured grid. +// gridobj: Task type of grid treatment. +// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc. +// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS. +// 2 -- Grid refinement. +// 3 -- Grid merging, merge two blocks into one block. +// 4 -- Grid deformation, achieve unstructured grid deformation. +// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells. +// 6 -- Grid mirroring, mirror a symmetry grid to whole grid. +// 7 -- Grid type change, convert structured grid to unstructured grid. // multiblock: Multi-block grid or not, only for structured grid conversion. // 0 -- Not. // 1 -- Yes. @@ -46,19 +47,24 @@ int gridobj = 1; int multiblock = 0; int iadapt = 0; int SymmetryFaceVector = 1; - int gridReorder = 0; int faceReorderMethod = 0; -// axisup: Type of Cartisien coordinates system, used in grid conversion. -// 1 -- Y upward. (default) -// 2 -- Z upward. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". // 0 -- Interface. (default) // 1 -- Physical boundary condition, used in Hybrid solver. int omit_no_bound_bc = 0; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ int dumpOldGrid = 0; // from_gfile: path of original data file for unstructure grid convert from. // out_gfile: path of target file for grid convert to, *.fts type of file usually. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ int fileformat = 0; // Parameters for hybrid solver. // mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type. -// mixgrid_str: path of structure grid file for hybrid solver, *.fts type. -string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; -string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; +// mixgrid_str: path of structure grid file for hybrid solver, *.fts type. +string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; +string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; // Some parameters for structured overlapping grid. int codeOfDigHoles = 1; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 2 -- refine structured grid. // maxproc: The number of partition zones that want to be divided into. // numberOfMultifile: The number of partition grid files that want to be dumped out. - int pgridtype = 0; int maxproc = 4; int numberOfMultifile = 1; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 0 -- Not. // 1 -- Yes. // blockIndexOfMark: the block index of mark, only for structured grid partition. -// cellIndexOfMark: the cell index of mark, only for structured grid partition. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +int cellIndexOfMark[] = [185, 30, 1]; -// parallel Strategy: -//! -# 0 : each zone is assigned to the one that defined in grid partition procedure. -//! -# 1 : random assigned for each zone or by some else ways. -int parallelStrategy = 1; +// parallelStrategy: +// 0 -- each zone is assigned to the one that defined in grid partition procedure. +// 1 -- random assigned for each zone or by some else ways. +int parallelStrategy = 1; //----------------------------------------------------------------------- # File path # //----------------------------------------------------------------------- -// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). +// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). // partition_grid_file: Target partition grid file(PHengLEI type, *.fts). string original_grid_file = "./grid/sphere_mixed.fts"; string partition_grid_file = "./grid/sphere_mixed__4.fts"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 1 -- perfect balance. // maxproc -- perfect imbalance. // 1.05 -- recommended. - int omit_no_bound_bc = 0; int npartmethod = 1; int parallelPartitionMethod = 2; -double parmetisBalance = 1.05; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ int numberOfMultigrid = 1; # Default parameters for CFD simulation # ######################################################################### // maxSimuStep: The max simulation step, don't care simulation is restart or not. -// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. -// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. +// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. +// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved. -// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. -// intervalStepRes: The step intervals for residual file 'res.dat' saved. -// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. -// 0 -- no precondition process. (default, mach > 0.3) -// 1 -- carry out precondition process. (mach number <= 0.3) - -int maxSimuStep = 20000; - -int intervalStepFlow = 1000; -int intervalStepPlot = 1000; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. +// 0 -- no precondition process. (default, mach > 0.3) +// 1 -- carry out precondition process. (mach number <= 0.3) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // freestream_vibration_temperature: Dimensional freestream vibration temperature. // refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition. // height: Fly height, unit of km. // wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition. -// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like: -// 1 dm = 0.1 m. -// 1 cm = 0.01 m. -// 1 mm = 0.001m. -// 1 inch = 0.0254m. -// 1 foot = 12 inches = 0.3048m. -// 1 yard = 3 feet = 0.9144m. +// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter. Common dimensions like: +// 1 dm = 0.1 m. +// 1 cm = 0.01 m. +// 1 mm = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit. // TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit. // radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary // condition is radiation equilibrium temperature, and 0.8 is the default value. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// refMolecularWeight: the reference molecular weight of gas used for perfect gas. The unit is g/mol. // Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on. - -int directionMethod = 0; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2). //double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)). -//int inflowParaType = 3; -//int nsubsonicInlet = 1; -//int nsubsonicOutlet = 1; -//string inLetFileName = "./bin/subsonicInlet.hypara"; -//string outLetFileName = "./bin/subsonicOutlet.hypara"; -//double refDimensionalTemperature = 288.144; -//double refDimensionalPressure = 1.01313E05; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ double forceReferenceArea = 1.0; // unit of meter^2. double TorqueRefX = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# Struct Solver * +#************************************************************************ // inviscidSchemeName: Spatial discretisation scheme of struct grid. // Using this when solve structered grid or hybrid. -// -- "vanleer", "steger", "hlle", "lax_f". -// -- "roe", "modified_roe". +// -- "vanleer", "steger", "hlle", "lax_f", +// -- "roe", "modified_roe", // -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+". // isWennScheme: If using WENN Scheme of struct grid. -// 0 -- NO. (default) -// 1 -- Yes. +// 0 -- NO. (default) +// 1 -- Yes. // str_limiter_name: Limiter of struct grid. -// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth". -// -- "nolim", no limiter. -// -- "vanalbada_clz", clz supersonic version. -// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3" - +// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth", +// -- "nolim", no limiter, +// -- "vanalbada_clz", clz supersonic version, +// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3". string inviscidSchemeName = "roe"; int isWennScheme = 0; -string str_limiter_name = "vanalbada"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 3 -- IDDES. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // Using this when solve Unstructered grid or hybrid. -// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "barth", "vencat", "vanleer", "minmod", +// -- "vanalbada", "smooth", "nnd", "lpz", "1st", // -- "nolim", no limiter. // uns_vis_name: Discretisation method of viscous term. // -- "std", "test", "aver", "new1", "new2". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "default", "ggcell", "ggnode", "lsq". // ivencat: Variation of vencat limiter. // 0 -- org method, it is independent of grid scale. // 1 -- new method, it is dependent of grid scale. @@ -442,18 +451,18 @@ string str_limiter_name = "vanalbada"; // 3 -- Harten type, which is default used. // roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0. // It is used to scale the default Roe entropy fix coefficients. -// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 1.0; // statisticalTimePeriod: Used as time period of statistic analysis. // when the value is negative, time period is treated as infinite. // statisticMethod: Statistic reynolds stress method. -// 0 -- tau = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // min_sub_iter: The min sub iteration of unsteady simulation. // max_sub_iter: The max sub iteration of unsteady simulation. // tol_sub_iter: The tolerance of sub iteration of unsteady simulation. // tscheme: Temporal Discretisation method. -// 1 -- Runge-Kutta Multi-State. -// 2 -- Point implicit. -// 3 -- Full implicit. -// 4 -- LU-SGS. -// 5 -- Block LU-SGS. -// 6 -- Jacobian iteration. -// 7 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // CFLStart: Started cfl number. // CFLEnd: End cfl number. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS. // ifLocalTimeStep: Time step method. -// 0 --Local. -// 1 --Global. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 0 -- global unified CFL number. +// 1 -- local CFL number. // isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no. // visl_min: Minimum value of laminar viscosity coefficient. // turbCFLScale: Turbulence model cfl number factor. // codeOfAleModel: Arbitrary Lagrangian-Eulerian method. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 0 -- no ALE method. +// 1 -- ALE method for non-moving grids. +// 2 -- ALE method for moving grids. +// 3 -- ALE method for deforming grids. // wallFunctionType: The type of wall function to implement. -// 0 -- no wall function. (default) -// 1 -- standard wall function. -// 2 -- Pab3D wall function. +// 0 -- no wall function. (default) +// 1 -- standard wall function. +// 2 -- Pab3D wall function. // RKStage: The number of Runge-Kutta step. // lamda: Cofficient of Runge-Kutta step. - -int iunsteady = 0; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2. int methodOfDualTime = 3; int min_sub_iter = 50; int max_sub_iter = 50; double tol_sub_iter = 0.01; -int tscheme = 4; +int tscheme = 4; int iSimplifyViscousTerm = 1; int ifLocalTimeStep = 0; int isUseLocalCFL = 0; int isUsePreTwall = 0; -double CFLStart = 0.01; -double CFLEnd = 10.0; -int CFLVaryStep = 500; - +double CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# File In or Out * +#************************************************************************ // numberOfGridGroups: The number of grid groups. // gridfile: The partitioned Grid file path, using relative path, // which is relative to the working directory. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps. // restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps. // turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps. -// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps. +// visualfile: The visualization file path of flowfield, write data for every default (intervalStepPlot) steps. // wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps. // nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. // nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. // nIsComputeWallDist: Whether to compute the wall distance. // 0 -- Compute wall distance. // 1 -- Not compute. -// -// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism. -// wall_heatfluxfile : The file to output the MaxHeatFlux of wall. - -int numberOfGridGroups = 1; -string gridfile = "./grid/rae2822_hybrid2d__4.fts"; -string wallTemperaturefile= ""; +// protectionFile0 and protectionFile1: Two continuation file of the data protection mechanism. +// wall_heatfluxfile: The file to output the MaxHeatFlux of wall. +int numberOfGridGroups = 1; +string gridfile = "./grid/rae2822_hybrid2d__4.fts"; +string wallTemperaturefile = ""; int nIsComputeWallDist = 0; int walldistMethod = 1; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), -// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52), -// -- overlap iblank(iblank, 81) - -// -- specific heat ratio(gama, 56) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11), -// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15) -// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19) -// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- heat flux of species diffusion term(Qs, 9), heat flux of vibrational temperature term(Qv, 10), heat flux of electron temperature term(Qe, 11), +// -- species mass fractions(Ns, 12), x component of wall velocity(Vx, 13), y component of wall velocity(Vy, 14), z component of wall velocity(Vz, 15), +// -- slip translational-rotational temperature(Tts, 16), slip vibrational temperature(Tvs, 17), slip electron temperature(Tes, 18), absolute wall velocity(Vs, 19), +// -- Stanton number(St, 20), coefficient of heat rate(Ch, 21), temperature jump(deltaT, 22), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ int dumpStandardModel = 0; // 1 -- Real cell where the probe is located. // nProbeVariables: Number of variables want to be dumped for probes monitered. // probeVariables : Variable types dumped, listed as following: -// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!! // probeVariables order must from small to big. // probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables. -// 0 -- Take the value of probe's cell as probe real value. -// 1 -- Interpolation from probe's and neighbouring cell to probe. -// 2 -- Interpolation from probe's cell nodes to probe. +// 0 -- Take the value of probe's cell as probe real value. +// 1 -- Interpolation from probe's and neighbouring cell to probe. +// 2 -- Interpolation from probe's cell nodes to probe. int ifSetDataMonitor = 0; -int dataMonitorType = 0; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// transitionType: transition model type // 0 -- none. // 2 -- gama-re-theta. -// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition -// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not - - +// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition. +// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not. int turbInterval = 1; int turbOrderStruct = 2; int kindOfTurbSource = 0; int mod_turb_res = 0; -double turb_relax = 1.0; double freeStreamViscosity = 1.0e-3; double muoo = 3.0; double kwoo = 5.0; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - not. +// = 1 -- Create LESSolver; +// != 1 -- not. // amplitudeofDisturb: Amplitude of adding disturb. // disturbstep: Unsteady time step or steady iteration of adding random disturb. // iterdisturb: Add random disturb in every sub-iter or only first sub-iter. -// = 0 - in only first sub-iter; -// != 0 - in every sub-iter. +// = 0 -- in only first sub-iter; +// != 0 -- in every sub-iter. // ipraddisturb: Add density and pressure disturb or not. // ibodyforce: Add body force in source flux of NS equations or not. -// = 0 - not; -// != 0 - Add body force. +// = 0 -- not; +// != 0 -- Add body force. // bodyforce: Body force in source flux of NS equations or not. // utau: friction velocity, using in DNSDisturb. // sgsmodel: subgrid scale model. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak); -// = 2 - pow(deltai * deltaj *deltak, 1/3); -// = 3 - Devloped by Scotti. -// wallDampingFunctionType: = 0 - no wall function; -// = 1 - van Driest; -// = 2 - developed by Dr. Deng Xiaobing; -// = 3 - developed by Piomelli. +// deltaFunctionType: = 1 -- MAX(deltai, deltaj, deltak); +// = 2 -- pow(deltai * deltaj *deltak, 1/3); +// = 3 -- Devloped by Scotti. +// wallDampingFunctionType: = 0 -- no wall function; +// = 1 -- van Driest; +// = 2 -- developed by Dr. Deng Xiaobing; +// = 3 -- developed by Piomelli. // turbViscousCutType: turbulent viscosity cut type. -// = 0 - mu_total = mut + mul; -// = 1 - mu_total = max(mut-mul,0)+ mul; -// = 2 - mu_total = max(mut ,0)+ mul. +// = 0 -- mu_total = mut + mul; +// = 1 -- mu_total = max(mut-mul, 0) + mul; +// = 2 -- mu_total = max(mut , 0) + mul. // smagConstant: constant of smagorinsky model. // waleConstant: constant of wale model. -// filterDirection[3]: filter variables in i, j, k direction or not. +// filterDirection [3]: filter variables in i, j, k direction or not. // averageDirection[3]: average variables in i, j, k direction or not. // isotropicConstant: constant of isotropic part of SGS stress. - int iLES = 0; string sgsmodel = "smagorinsky"; int deltaFunctionType = 2; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# Other Parameters for Hypersonic Non-equilibrium Gas * +#************************************************************************ // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: // 0 -- gas model is fixed in the codes. // 1 -- gas model is imported from library files. -// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver, -// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver. -// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps. -// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // nIdealState: whether take all gas species as ideal gas for gas-mixture process. // 0 -- No. -// 1 -- Yes. -// nTEnergyModel: the method to computing temperature energy model. +// 1 -- Yes. // nTEnergyModel: the method to computing temperature energy model. // 0 -- the energy term is computed using the conventional method. // 1 -- the energy term is computed using the polynomial fitting method. // 2 -- the energy term is computed using the piecewise polynomial fitting method. // parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model. // The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value. // catalyticCoef: -// 0.0 -- full non-catalytic wall boundary condition. -// 1.0 -- full catalytic wall boundary condition. -// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// nTemperatureJump : the method to calculate the temperature jump. -// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode. -// 1 -- the general method where the iteration is calculated with the translation-rotation temperature. -// nSurfGradMethod : the method to compute the surface heating ratio. -// 0 -- the gradient of variable is computed with the first-order difference method. -// 1 -- the gradient of variable is computed with the Green-Guass integral method. -// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero. -// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes. -// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value. -// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping. +// 0.0 -- full non-catalytic wall boundary condition. +// 1.0 -- full catalytic wall boundary condition. +// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// nTemperatureJump: the method to calculate the temperature jump. +// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode. +// 1 -- the general method where the iteration is calculated with the translation-rotation temperature. +// nSurfGradMethod: the method to compute the surface heating ratio. +// 0 -- the gradient of variable is computed with the first-order difference method. +// 1 -- the gradient of variable is computed with the Green-Guass integral method. +// nRapidFlowfield: initialize the flowfield using the rapid engineering method when it is greater than zero. +// nSurfHeatMonitor: To exam the surface heating change or not. 0 is no, 1 is yes. +// nInitPressureStep: the steps to initialize the boundary variables when the rapid method is used. 100 is the default value. +// nDumpCFLNumber: 1 indicates dumping the CFL number to file, 0 denotes no dumping. // sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0]. // sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0]. // sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// spectrumRadiusCoef: The value is in range of [0.0, 2.0]. -// staticPressureRelaxCorf: The value is in range of [0.1, 1.0]. -// nIsChemicalFreeze : the flag to freeze the chemical reactions. -// 0 -- not freeze, the chemical reaction sources will be calculated. -// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te - -//maxViscous: the maximum of Viscous. -//trTemperatureMin: the minimum value of trTemperature. -//veTemperatureMin: the minimum value of veTemperature. -//densityMin: the minimum value of density. -//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0]. -// nDebug: cout the Wrong place and abort -// 0 -- not used. -// 1 -- used. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// spectrumRadiusCoef: The value is in range of [0.0, 2.0]. +// staticPressureRelaxCorf: The value is in range of [0.1, 1.0]. +// nIsChemicalFreeze: the flag to freeze the chemical reactions. +// 0 -- not freeze, the chemical reaction sources will be calculated. +// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated. +// veTemperatureMin: The minimum of Tv and Te. +// maxViscous: the maximum of Viscous. +// trTemperatureMin: the minimum value of trTemperature. +// veTemperatureMin: the minimum value of veTemperature. +// densityMin: the minimum value of density. +// tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0]. +// nDebug: cout the Wrong place and abort +// 0 -- not used. +// 1 -- used. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid -// 0 -- not used. -// 1 -- used. -// nViscosityPeModified: Pe Modified for ViscosityCoef -// 0 -- not used. -// 1 -- used. -// nChemcalSourceModified: Modified on ChemcalSource -// 0 -- not used. -// 1 -- used. -// nChemcalSourceEsMethod: Modified on ChemcalSource -// 0 -- approximation algorithm 1 (Ori.) -// 1 -- approximation algorithm 2 (New) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid. +// 0 -- not used. +// 1 -- used. +// nViscosityPeModified: Pe Modified for ViscosityCoef. +// 0 -- not used. +// 1 -- used. +// nChemcalSourceModified: Modified on ChemcalSource. +// 0 -- not used. +// 1 -- used. +// nChemcalSourceEsMethod: Modified on ChemcalSource. +// 0 -- approximation algorithm 1 (Ori). +// 1 -- approximation algorithm 2 (New). // nMaxStepTemperature: the iterative steps of temperature. - -// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs -// 0 -- not used -// 1 -- used - -// nDiagonalModified: Modified on Diagonal -// 0 -- not used -// 1 -- Ori. -// 2 -- new - -//nGradPrimtiveMethod: -// 0 -- Ori. -// 1 -- new +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 0 -- Blottner fitting method(N89). +// 1 -- Gupta fitting method(N90). // nContinueModel: The new continue model can switch different computation model. -// 0 -- Not use the new continue model. -// 1 -- use the new continue model. +// 0 -- Not use the new continue model. +// 1 -- use the new continue model. // nSutherland: -// 0 -- stands for selecting the Blotter curve fits mode. -// 1 -- stands for Sutherland relation. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11". -// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. -// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. -// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. -// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 NO CO CO2 H2 N2 Air CH4. -// For self-definition model, the gasfile is used to indicate the file path of the new gas model. +// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. +// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. +// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "Gas-Mixture" -- indicates the process of mixing gas without reacting. +// for struct solver mixing two species��SpeciesA, SpeciesB��. +// for unstruct solver mixing multi-species��O2 NO CO CO2 H2 N2 Air CH4��. +// For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. // ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes. -// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation. -// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation. -// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation. -// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory. -// 0 -- no, -// 1 -- yes. +// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation. +// nIterSecondStep: the maximum number of iteration in the second step for the self-adaptive calculation. +// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation. +// nEnergyAssembly: the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory. +// 0 -- no, +// 1 -- yes. // nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model. -// 0 -- the density. -// 1 -- the translation temperature. -// 2 -- the vibration temperature. -// 3 -- the electron temperature. -// 4 -- the pressure. -// 5 -- the mass fraction of oxygen. -// 6 -- the mass fraction of nitrogen. +// 0 -- the density. +// 1 -- the translation temperature. +// 2 -- the vibration temperature. +// 3 -- the electron temperature. +// 4 -- the pressure. +// 5 -- the mass fraction of oxygen. +// 6 -- the mass fraction of nitrogen. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. -// useHyflowSetting : Setting for HyFLOW GUI. -// 0 -- PHengLEI -// 1 -- HyFLOW -// nProtectData : Use the continuation file data protection mechanism. -// 0 -- no -// 1 -- yes - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +double refGama = 1.4; +double prl = 0.72; +double prt = 0.90; +double sc_l = 0.5; +double sc_t = 0.5; -int nGasModel = 0; -int nchem = 0; -int nchemsrc = 1; -int nchemrad = 1; -int ntmodel = 1; +int nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 0; -int nDebug = 0; -int nSpeciesLimit = 1; -int nTurblenceForChemical = 0; -int nViscosityFluxSublevelModified = 1; -int nViscosityPeModified = 0; -int nChemcalSourceModified = 2; -int nChemcalSourceEsMethod = 1; -int nMaxStepTemperature = 5; -int veTemperatureMinModified = 1; -int nDiagonalModified = 0; -int nGradPrimtiveMethod = 1; -int nInviscidFluxModify = 1; -int nQlLimitMethod = 2; -int nSpeciesForWallMethod = 1; -int nDensityForWallMethod = 0; +int nDebug = 0; +int nSpeciesLimit = 1; +int nTurblenceForChemical = 0; +int nViscosityFluxSublevelModified = 1; +int nViscosityPeModified = 0; +int nChemcalSourceModified = 2; +int nChemcalSourceEsMethod = 1; +int nMaxStepTemperature = 5; +int veTemperatureMinModified = 1; +int nDiagonalModified = 0; +int nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; //string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; //string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; -//string gasfile = "Pa"; +//string gasfile = "Pa"; //string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ int ismooth_turb = 0; int SAProductType = 2; // ----------------- Overset Grid parameter ----------------------------- -int codeOfDigHoles = 1; -int codeOfTurbulentModel = 0; -string masterFileName = "./grid/searchFile.inp"; -string holeBasicFileName = "./grid/holeBasicFile.inp"; -string holeFullFileName = "./grid/holeFullFile.dat"; -string linkFileName = "./grid/topology.dat"; -string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; +int codeOfDigHoles = 1; +int codeOfTurbulentModel = 0; +string masterFileName = "./grid/searchFile.inp"; +string holeBasicFileName = "./grid/holeBasicFile.inp"; +string holeFullFileName = "./grid/holeFullFile.dat"; +string linkFileName = "./grid/topology.dat"; +string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; -######################################################################### -# High Order Struct Solver # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 0 -- NSSolverStruct using Finite Volume Method. +// 1 -- NSSolverStruct using Finite Differ Method. // SolverStructOrder: Spatial discretisation order of NS equations with struct grid. // <= 2 -- finite volume method. // >= 3 -- finite difference order. (to be completed) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.ovs"; -double walldistMainZone = 1.0 -double toleranceForOversetSearch = 1.0e-3; -double toleranceForOversetBox = 1.0e-3; -int twoOrderInterpolationOrNot = 0; -int keyEnlargeOfActiveNodes = 0; -int outTecplotOverset = 0; -int outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.ovs"; +double walldistMainZone = 1.0 +double toleranceForOversetSearch = 1.0e-3; +double toleranceForOversetBox = 1.0e-3; +int twoOrderInterpolationOrNot = 0; +int keyEnlargeOfActiveNodes = 0; +int outTecplotOverset = 0; +int outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ double referenceLength = 1.0; double referenceVelocity = 1.0; double referenceDensity = 1.0; -int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd; -int strategyForGCLSource = 0; //0-present; 1-Ahn; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +int RBDMethod_0 = 0; +double amplitude_0 = 0.0; +double reduceFrequency_0 = 0.0; +// direction of rotation. // 1 -- clockwise from the point of view along the positive x axis. // -1 -- anticlockwise from the point of view along the positive x axis. -int direction_0 = -1; -double rotateFrequency_0 = 0.0; -//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; -//additional force (system axis) fX fY fZ -double addedForce_0[] = 0.0 ,0.0 ,0.0 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/L03_ThreeD_Poiseuille_MRT_MPI_4CPU/bin/input.txt b/L03_ThreeD_Poiseuille_MRT_MPI_4CPU/bin/input.txt new file mode 100644 index 0000000..ec63d5b --- /dev/null +++ b/L03_ThreeD_Poiseuille_MRT_MPI_4CPU/bin/input.txt @@ -0,0 +1,35 @@ +1 ！MRT set 1, BGK set 0 +0 continue.plt ！CONTI, resume :1 , new 0 //follows input datafile name //use ASCII文件 continue.plt +0 ！LES yes: 1 , no: 0 +0 mesh_3d.dat ！GEO read complex geo? yes:1, no:0 //follows input datafile name +0 ! MB multiblock LBM? yes:1, no:0 +1 2e-3 !CONV using converge criterion? yes:1, no:0 +100 ！NX +100 ! NY +100 ! NZ +1 ！ NX2 +1 ！ NY2 +1 ! NZ2 +0 ! LowX +0 ! LowY +0 ! LowZ +2 ! x_np +2 ! y_np +1 ! z_np +500 ! framerate +50000 ！total steps to terminate +1.0 ! density +0.6 ！ tau +(2.2e-7,0.0,0.0) ！ Volumetric force +D3Q19 ! velocity set +Poiseuille ! boundary condition +! note: in the following, boundary types: periodic,velocity, pressure +! are allowed. if "velocity" is applied, please strictly follow the format "velocity (%lf, %lf, %lf)". +periodic ！xmin face +periodic ！xmax face +periodic ！ymin face +periodic ！ymax face, +nonslip ！zmin face +nonslip ！zmax face +-------------------！ initial velocity field +(0.0, 0.00, 0.0) \ No newline at end of file diff --git a/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/key.hypara b/L03_ThreeD_Poiseuille_MRT_MPI_4CPU/bin/key.hypara similarity index 91% rename from H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/key.hypara rename to L03_ThreeD_Poiseuille_MRT_MPI_4CPU/bin/key.hypara index 80060fd..1a572c7 100644 --- a/H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU/bin/key.hypara +++ b/L03_ThreeD_Poiseuille_MRT_MPI_4CPU/bin/key.hypara @@ -17,12 +17,12 @@ string defaultParaFile = "./bin/cfd_para.hypara"; int ndim = 3; int nparafile = 1; -int nsimutask = 0; -string parafilename = "./bin/cfd_para_incompressible.hypara" +//int nsimutask = 0; //string parafilename = "./bin/cfd_para_subsonic.hypara"; //string parafilename = "./bin/cfd_para_transonic.hypara"; //string parafilename = "./bin/cfd_para_supersonic.hypara"; //string parafilename = "./bin/cfd_para_hypersonic.hypara"; +//string parafilename = "./bin/cfd_para_incompressible.hypara"; //int nsimutask = 1; //string parafilename = "./bin/grid_para.hypara"; @@ -39,6 +39,9 @@ string parafilename = "./bin/cfd_para_incompressible.hypara" //int nsimutask = 1; //string parafilename = "./bin/grid_refine_para.hypara"; +int nsimutask = 13; +string parafilename = "./bin/cfd_para.hypara"; + //int nsimutask = 14; //string parafilename = "./bin/integrative_solver.hypara"; diff --git a/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/cfd_para.hypara b/L04_ThreeD_Spoiler_BGK_MPI_8CPU/bin/cfd_para.hypara similarity index 60% rename from H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/cfd_para.hypara rename to L04_ThreeD_Spoiler_BGK_MPI_8CPU/bin/cfd_para.hypara index c344658..f903a5a 100644 --- a/H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU/bin/cfd_para.hypara +++ b/L04_ThreeD_Spoiler_BGK_MPI_8CPU/bin/cfd_para.hypara @@ -8,23 +8,24 @@ // Platform for Hybrid Engineering Simulation of Flows + // China Aerodynamics Research and Development Center + // (C) Copyright, Since 2010 + +// PHengLEI 2212 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### # Default parameters for Grid conversion # ########################################################################### // gridtype: Grid type for generation, conversion, reconstruction, merging. -// 0 -- Unstructured grid. -// 1 -- Structured grid. -// 2 -- Hybrid grid, include both of unstructured and structured grid. -// gridobj: Task type of grid treatment. -// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc. -// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS. -// 2 -- Grid refinement. -// 3 -- Grid merging, merge two blocks into one block. -// 4 -- Grid deformation, achieve unstructured grid deformation. -// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells. -// 6 -- Grid mirroring, mirror a symmetry grid to whole grid. -// 7 -- Grid type change, convert structured grid to unstructured grid. +// 0 -- Unstructured grid. +// 1 -- Structured grid. +// 2 -- Hybrid grid, include both of unstructured and structured grid. +// gridobj: Task type of grid treatment. +// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc. +// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS. +// 2 -- Grid refinement. +// 3 -- Grid merging, merge two blocks into one block. +// 4 -- Grid deformation, achieve unstructured grid deformation. +// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells. +// 6 -- Grid mirroring, mirror a symmetry grid to whole grid. +// 7 -- Grid type change, convert structured grid to unstructured grid. // multiblock: Multi-block grid or not, only for structured grid conversion. // 0 -- Not. // 1 -- Yes. @@ -46,19 +47,24 @@ int gridobj = 1; int multiblock = 0; int iadapt = 0; int SymmetryFaceVector = 1; - int gridReorder = 0; int faceReorderMethod = 0; -// axisup: Type of Cartisien coordinates system, used in grid conversion. -// 1 -- Y upward. (default) -// 2 -- Z upward. -int axisup = 1; +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; // omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". // 0 -- Interface. (default) // 1 -- Physical boundary condition, used in Hybrid solver. int omit_no_bound_bc = 0; +int omitRepeatInterface = 1; //----------------------------------------------------------------------- # Grid data type # @@ -87,10 +93,9 @@ int dumpOldGrid = 0; // from_gfile: path of original data file for unstructure grid convert from. // out_gfile: path of target file for grid convert to, *.fts type of file usually. int numberOfGridFile = 1; -string from_gfile = "./grid/rae2822_hybrid2d.cas"; -string from_gfile1= ""; - -string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; // ----------------- some advanced choices ------------------------------ // iunsteady: The Grid is for unsteady simulation or not. @@ -103,9 +108,9 @@ int fileformat = 0; // Parameters for hybrid solver. // mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type. -// mixgrid_str: path of structure grid file for hybrid solver, *.fts type. -string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; -string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; +// mixgrid_str: path of structure grid file for hybrid solver, *.fts type. +string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; +string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; // Some parameters for structured overlapping grid. int codeOfDigHoles = 1; @@ -119,31 +124,31 @@ string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; // 0 -- Not. (default) // 1 -- Yes. // geometryUnit: Geometry unit. -// 1 -- meter. -// 2 -- millimeter. -// 3 -- inch. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. // exclusiveCase: Parallel projection exclusive case. -// 0 -- NON case. -// 1 -- JSM-C2-NPOFF case. -// 2 -- CHNT. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. // projectOrgPoint: If the original wall points need to be projected or not. -int anisoRefine = 0; -int geometryUnit = 1; -int isProject = 0; -int readDist = 0; -int isDeform = 0; +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; int exclusiveCase = 0; int projectOrgPoint = 0; string geometryFileName = "./grid/jsm.igs"; // ----------------- Grid Deform Parameters ----------------------------- // deformationMethod: Grid Deform. -// 1 -- SPRING. -// 2 -- RBF. +// 1 -- SPRING. +// 2 -- RBF. // stationalGridFile: Original grid file. // visualFileName : The visualization file path of deform grid. // nDeformStep : The max deform step. -// flapAngle : The max flap angle. +// flapAngle : The max flap angle. // rotatePostionZ : Rotate postion. // rotatePostionY : Rotate postion. // gridSlice : If dump slice grid. @@ -163,10 +168,10 @@ int sliceAxis = 1; double slicePosition = 13; // ----------------- RBF Parameters ------------------------------------- -// numberOfReferenceCP : Number of reference Control Points. -// influencePara : The RBF influence radius parameter. +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. int numberOfReferenceCP = 40; -double influencePara = 25.0; +double influencePara = 25.0; // ----------------- Periodic Parameters -------------------------------- // Notice: Rotational periodicity only support rotation along the X axis! @@ -178,9 +183,8 @@ double influencePara = 25.0; which only support one direction. // rotationAngle: The relative angle between two periodic face. which is recorded in degrees. - int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; +double translationLength[] = [0.0, 0.0, 0.0]; double rotationAngle = 0.0; ######################################################################### @@ -192,7 +196,6 @@ double rotationAngle = 0.0; // 2 -- refine structured grid. // maxproc: The number of partition zones that want to be divided into. // numberOfMultifile: The number of partition grid files that want to be dumped out. - int pgridtype = 0; int maxproc = 4; int numberOfMultifile = 1; @@ -201,20 +204,20 @@ int numberOfMultifile = 1; // 0 -- Not. // 1 -- Yes. // blockIndexOfMark: the block index of mark, only for structured grid partition. -// cellIndexOfMark: the cell index of mark, only for structured grid partition. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. int traceMark = 0; int blockIndexOfMark = 0; -int cellIndexOfMark[] = [185,30,1]; +int cellIndexOfMark[] = [185, 30, 1]; -// parallel Strategy: -//! -# 0 : each zone is assigned to the one that defined in grid partition procedure. -//! -# 1 : random assigned for each zone or by some else ways. -int parallelStrategy = 1; +// parallelStrategy: +// 0 -- each zone is assigned to the one that defined in grid partition procedure. +// 1 -- random assigned for each zone or by some else ways. +int parallelStrategy = 1; //----------------------------------------------------------------------- # File path # //----------------------------------------------------------------------- -// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). +// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). // partition_grid_file: Target partition grid file(PHengLEI type, *.fts). string original_grid_file = "./grid/sphere_mixed.fts"; string partition_grid_file = "./grid/sphere_mixed__4.fts"; @@ -232,11 +235,10 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts"; // 1 -- perfect balance. // maxproc -- perfect imbalance. // 1.05 -- recommended. - int omit_no_bound_bc = 0; int npartmethod = 1; int parallelPartitionMethod = 2; -double parmetisBalance = 1.05; +double parmetisBalance = 1.05; // numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. // 1 -- single level. @@ -248,29 +250,35 @@ int numberOfMultigrid = 1; # Default parameters for CFD simulation # ######################################################################### // maxSimuStep: The max simulation step, don't care simulation is restart or not. -// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. -// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. +// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. +// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. // intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved. -// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. -// intervalStepRes: The step intervals for residual file 'res.dat' saved. -// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. -// 0 -- no precondition process. (default, mach > 0.3) -// 1 -- carry out precondition process. (mach number <= 0.3) - -int maxSimuStep = 20000; - -int intervalStepFlow = 1000; -int intervalStepPlot = 1000; +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) int compressible = 1; +// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. +// 0 -- no precondition process. (default, mach > 0.3) +// 1 -- carry out precondition process. (mach number <= 0.3) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + //----------------------------------------------------------------------- # CFD Control Parameter # //----------------------------------------------------------------------- @@ -281,33 +289,36 @@ int compressible = 1; // 0 -- the nondimensional conditions. // 1 -- the flight conditions. // 2 -- the experiment conditions. -// 3 -- the subsonic boundary conditions. +// 3 -- the subsonic boundary conditions. (Useless!) // 4 -- the condition that the velocity, temperature and density are given. // 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. // refReNumber: Reynolds number, which is based unit length, unit of 1/m. // refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. // freestream_vibration_temperature: Dimensional freestream vibration temperature. // refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition. // height: Fly height, unit of km. // wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition. -// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like: -// 1 dm = 0.1 m. -// 1 cm = 0.01 m. -// 1 mm = 0.001m. -// 1 inch = 0.0254m. -// 1 foot = 12 inches = 0.3048m. -// 1 yard = 3 feet = 0.9144m. +// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter. Common dimensions like: +// 1 dm = 0.1 m. +// 1 cm = 0.01 m. +// 1 mm = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. // forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit. // TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit. // radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary // condition is radiation equilibrium temperature, and 0.8 is the default value. -// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// refMolecularWeight: the reference molecular weight of gas used for perfect gas. The unit is g/mol. // Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on. - -int directionMethod = 0; +int directionMethod = 0; double refMachNumber = 0.73; double attackd = 2.79; double angleSlide = 0.00; +int flowInitMethod = 0; int inflowParaType = 0; double refReNumber = 6.5e6; @@ -321,29 +332,27 @@ double freestream_vibration_temperature = 300.00; //double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2). //double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)). -//int inflowParaType = 3; -//int nsubsonicInlet = 1; -//int nsubsonicOutlet = 1; -//string inLetFileName = "./bin/subsonicInlet.hypara"; -//string outLetFileName = "./bin/subsonicOutlet.hypara"; -//double refDimensionalTemperature = 288.144; -//double refDimensionalPressure = 1.01313E05; - -//The velocity, temperature and density are fixed. +// The velocity, temperature and density are fixed. //int inflowParaType = 4; //double refDimensionalVelocity = 1000.0; -//double refDimensionalDensity = 1.0e3; +//double refDimensionalDensity = 1.0e3; -//The velocity, temperature and pressure are fixed. +// The velocity, temperature and pressure are fixed. //int inflowParaType = 5; //double refDimensionalVelocity = 1000.0; //double refDimensionalPressure = 1.0e5; -//The MachNumber, temperature and pressure are fixed. +// The MachNumber, temperature and pressure are fixed. //int inflowParaType = 6; -//double refDimensionalTemperature = 293; +//double refDimensionalTemperature = 293.0; //double refDimensionalPressure = 8886.06; +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + double wallTemperature = -1.0; double radiationCoef = 0.8; @@ -357,41 +366,41 @@ double forceReferenceArea = 1.0; // unit of meter^2. double TorqueRefX = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter. +double knudsenLength = 1.0; // unit of meter. double refMolecularWeight = 28.9644; // unit of g/mol. //----------------------------------------------------------------------- # Spatial Discretisation # //----------------------------------------------------------------------- -#******************************************************************* -# Struct Solver * -#******************************************************************* +#************************************************************************ +# Struct Solver * +#************************************************************************ // inviscidSchemeName: Spatial discretisation scheme of struct grid. // Using this when solve structered grid or hybrid. -// -- "vanleer", "steger", "hlle", "lax_f". -// -- "roe", "modified_roe". +// -- "vanleer", "steger", "hlle", "lax_f", +// -- "roe", "modified_roe", // -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+". // isWennScheme: If using WENN Scheme of struct grid. -// 0 -- NO. (default) -// 1 -- Yes. +// 0 -- NO. (default) +// 1 -- Yes. // str_limiter_name: Limiter of struct grid. -// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth". -// -- "nolim", no limiter. -// -- "vanalbada_clz", clz supersonic version. -// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3" - +// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth", +// -- "nolim", no limiter, +// -- "vanalbada_clz", clz supersonic version, +// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3". string inviscidSchemeName = "roe"; int isWennScheme = 0; -string str_limiter_name = "vanalbada"; +string str_limiter_name = "vanalbada"; -#******************************************************************* -# UnStruct Solver or Common * -#******************************************************************* +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ // viscousType: Viscous model. -// 0 -- Euler. -// 1 -- Lamilar. -// 2 -- Algebraic. -// 3 -- 1eq turbulent. -// 4 -- 2eq turbulent. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. // viscousName: Laminar or tubulent model. // -- "0eq-bl". // -- "1eq-sa". @@ -410,16 +419,16 @@ string str_limiter_name = "vanalbada"; // 3 -- IDDES. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid. // Using this when solve Unstructered grid or hybrid. -// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle". +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", // -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". // uns_limiter_name: Limiter of Unstruct grid. -// -- "barth", "vencat", "vanleer", "minmod". -// -- "vanalbada", "smooth", "nnd", "lpz", "1st". +// -- "barth", "vencat", "vanleer", "minmod", +// -- "vanalbada", "smooth", "nnd", "lpz", "1st", // -- "nolim", no limiter. // uns_vis_name: Discretisation method of viscous term. // -- "std", "test", "aver", "new1", "new2". // gradientName: Gradient reconstruction method. -// -- "default", "ggcell", "ggnode", "lsq". +// -- "default", "ggcell", "ggnode", "lsq". // ivencat: Variation of vencat limiter. // 0 -- org method, it is independent of grid scale. // 1 -- new method, it is dependent of grid scale. @@ -442,18 +451,18 @@ string str_limiter_name = "vanalbada"; // 3 -- Harten type, which is default used. // roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0. // It is used to scale the default Roe entropy fix coefficients. -// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0 +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. -//int viscousType = 0; +//int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; +//int viscousType = 1; //string viscousName = "laminar"; -int viscousType = 3; +int viscousType = 3; string viscousName = "1eq-sa"; -//int viscousType = 4; +//int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; int DESType = 0; @@ -463,7 +472,7 @@ string uns_limiter_name = "vencat"; string uns_vis_name = "test"; string gradientName = "ggnode"; -int ivencat = 7; +int ivencat = 7; double venkatCoeff = 5.0; int reconmeth = 1; int limitVariables = 0; @@ -475,9 +484,9 @@ double roeEntropyScale = 1.0; double AusmpwPlusLimiter = 1.0; -//----------------------------------------------------------------------- -# Temporal Discretisation # -//----------------------------------------------------------------------- +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ // iunsteady: Steady or unsteady. // 0 -- steady. // 1 -- unsteay. @@ -490,51 +499,57 @@ double AusmpwPlusLimiter = 1.0; // statisticalTimePeriod: Used as time period of statistic analysis. // when the value is negative, time period is treated as infinite. // statisticMethod: Statistic reynolds stress method. -// 0 -- tau = - ^2 -// 1 -- tau = +// 0 -- tau = - ^2 +// 1 -- tau = // min_sub_iter: The min sub iteration of unsteady simulation. // max_sub_iter: The max sub iteration of unsteady simulation. // tol_sub_iter: The tolerance of sub iteration of unsteady simulation. // tscheme: Temporal Discretisation method. -// 1 -- Runge-Kutta Multi-State. -// 2 -- Point implicit. -// 3 -- Full implicit. -// 4 -- LU-SGS. -// 5 -- Block LU-SGS. -// 6 -- Jacobian iteration. -// 7 -- Line LU-SGS. -// 8 -- Matrix LU-SGS. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. // iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. // Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. // CFLStart: Started cfl number. // CFLEnd: End cfl number. // CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. // ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) // swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. // nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. // LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS. // ifLocalTimeStep: Time step method. -// 0 --Local. -// 1 --Global. +// 0 --Local. +// 1 --Global. // isUseLocalCFL: use variable number of CFL or not. -// 0 -- global unified CFL number. -// 1 -- local CFL number. +// 0 -- global unified CFL number. +// 1 -- local CFL number. // isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no. // visl_min: Minimum value of laminar viscosity coefficient. // turbCFLScale: Turbulence model cfl number factor. // codeOfAleModel: Arbitrary Lagrangian-Eulerian method. -// 0 -- no ALE method. -// 1 -- ALE method for non-moving grids. -// 2 -- ALE method for moving grids. -// 3 -- ALE method for deforming grids. +// 0 -- no ALE method. +// 1 -- ALE method for non-moving grids. +// 2 -- ALE method for moving grids. +// 3 -- ALE method for deforming grids. // wallFunctionType: The type of wall function to implement. -// 0 -- no wall function. (default) -// 1 -- standard wall function. -// 2 -- Pab3D wall function. +// 0 -- no wall function. (default) +// 1 -- standard wall function. +// 2 -- Pab3D wall function. // RKStage: The number of Runge-Kutta step. // lamda: Cofficient of Runge-Kutta step. - -int iunsteady = 0; +int iunsteady = 0; double physicalTimeStep = 0.01; double physicalTimeStepDimensional = -0.001; int ifStartFromSteadyResults = 0; @@ -543,39 +558,42 @@ int ifStaticsReynoldsStress = 0; int startStatisticStep = 800000; double statisticalTimePeriod = -1.0; int statisticMethod = 0; -int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2; +int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2. int methodOfDualTime = 3; int min_sub_iter = 50; int max_sub_iter = 50; double tol_sub_iter = 0.01; -int tscheme = 4; +int tscheme = 4; int iSimplifyViscousTerm = 1; int ifLocalTimeStep = 0; int isUseLocalCFL = 0; int isUsePreTwall = 0; -double CFLStart = 0.01; -double CFLEnd = 10.0; -int CFLVaryStep = 500; - +double CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; double pMaxForCFL = 0.2; double pMinForCFL = 0.1; double deltaMaxForCFL = 0.2; double magnifyFactorForCFL = 1.1; double reduceFactorForCFL = 0.5; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; int nLUSGSSweeps = 1; double LUSGSTolerance = 0.01; -int order = 2; +int order = 2; double visl_min = 0.01; double turbCFLScale = 1.0; -double csrv = 2.0; +double csrv = 1.0; double timemax = 1.0e10; double dtsave = -1.0; int maxale = 10; @@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0]; //int RKStage = 4; //double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; - -//----------------------------------------------------------------------- -# File In or Out # -//----------------------------------------------------------------------- +#************************************************************************ +# File In or Out * +#************************************************************************ // numberOfGridGroups: The number of grid groups. // gridfile: The partitioned Grid file path, using relative path, // which is relative to the working directory. @@ -611,20 +628,18 @@ double lamda[] = [0.5, 1.0]; // aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps. // restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps. // turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps. -// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps. +// visualfile: The visualization file path of flowfield, write data for every default (intervalStepPlot) steps. // wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps. // nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. // nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. // nIsComputeWallDist: Whether to compute the wall distance. // 0 -- Compute wall distance. // 1 -- Not compute. -// -// protectionFile0 and protectionFile1 : Two continuation file of the data protection mechanism. -// wall_heatfluxfile : The file to output the MaxHeatFlux of wall. - -int numberOfGridGroups = 1; -string gridfile = "./grid/rae2822_hybrid2d__4.fts"; -string wallTemperaturefile= ""; +// protectionFile0 and protectionFile1: Two continuation file of the data protection mechanism. +// wall_heatfluxfile: The file to output the MaxHeatFlux of wall. +int numberOfGridGroups = 1; +string gridfile = "./grid/rae2822_hybrid2d__4.fts"; +string wallTemperaturefile = ""; int nIsComputeWallDist = 0; int walldistMethod = 1; @@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0; string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; string aircoeffile = "results/aircoef.dat"; string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; string visualfile = "results/tecflow.plt"; string wall_aircoefile = "results/wall_aircoef.dat"; @@ -645,10 +662,14 @@ string protectionFile0 = "results/flow0.dat"; string protectionFile1 = "results/flow1.dat"; string wall_heatfluxfile = "results/wall_heatflux.dat"; -int nDumpSurfaceInfo = 0; -string wall_varfile = ""; +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; -string jetDefineFile = "bin/jet.hypara"; +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; string sixDofFileName = "results/sixDofInfo.dat"; string derivativeFileName = "results/identify.dat"; @@ -659,7 +680,8 @@ int plotFieldType = 0; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. // 1 -- Tecplot ASCII. - +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. int visualfileType = 1; // samplefileMode: The dump mode of sample file. @@ -697,21 +719,21 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), // -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), -// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52), -// -- overlap iblank(iblank, 81) - -// -- specific heat ratio(gama, 56) +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). // Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! // Variables order must from small to big. //-----------the optional parameters list for the wall boundary condition---------------- // nVisualWallVariables: The number of visual variables on wall. // visualWallVariables : dumped variable types, listed as following: -// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4), -// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8), -// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11), -// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15) -// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19) -// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23) +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- heat flux of species diffusion term(Qs, 9), heat flux of vibrational temperature term(Qv, 10), heat flux of electron temperature term(Qe, 11), +// -- species mass fractions(Ns, 12), x component of wall velocity(Vx, 13), y component of wall velocity(Vy, 14), z component of wall velocity(Vz, 15), +// -- slip translational-rotational temperature(Tts, 16), slip vibrational temperature(Tvs, 17), slip electron temperature(Tes, 18), absolute wall velocity(Vs, 19), +// -- Stanton number(St, 20), coefficient of heat rate(Ch, 21), temperature jump(deltaT, 22), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). int nVisualVariables = 8; int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; @@ -739,16 +761,18 @@ int dumpStandardModel = 0; // 1 -- Real cell where the probe is located. // nProbeVariables: Number of variables want to be dumped for probes monitered. // probeVariables : Variable types dumped, listed as following: -// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6). +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). // Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!! // probeVariables order must from small to big. // probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables. -// 0 -- Take the value of probe's cell as probe real value. -// 1 -- Interpolation from probe's and neighbouring cell to probe. -// 2 -- Interpolation from probe's cell nodes to probe. +// 0 -- Take the value of probe's cell as probe real value. +// 1 -- Interpolation from probe's and neighbouring cell to probe. +// 2 -- Interpolation from probe's cell nodes to probe. int ifSetDataMonitor = 0; -int dataMonitorType = 0; +int dataMonitorType = 0; string probesDefineFile = "bin/probes_XYZ.dat"; //int dataMonitorType = 1; @@ -761,28 +785,26 @@ string probesDefineFile = "bin/probes_XYZ.dat"; int searchCellsMethod = 0; -int nProbeVariables = 7; -int probeVariables[] = [0, 1, 2, 3, 4, 5, 6]; -int probeVariablesInterpolationMethod = 0; -//----------------------------------------------------------------------- -# Turbulence Parameter # -//----------------------------------------------------------------------- +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ // turbInterval: Iteration number of turbulence. // kindOfTurbSource: Kinds of turbulent source. // 0 -- Original. // mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. -// transitionType: transition model type +// transitionType: transition model type // 0 -- none. // 2 -- gama-re-theta. -// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition -// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not - - +// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition. +// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not. int turbInterval = 1; int turbOrderStruct = 2; int kindOfTurbSource = 0; int mod_turb_res = 0; -double turb_relax = 1.0; double freeStreamViscosity = 1.0e-3; double muoo = 3.0; double kwoo = 5.0; @@ -790,29 +812,28 @@ int transitionType = 0; double turbIntensity = -1.0; int freeturbIntensitySRModify = 0; double freeDecayXLocation = 0.0; -int compressibleCorrection = 0; -int prandtlNumberCorrection = 0; +int compressibleCorrection = 0; int transitionMaFix = 1; -# maximum eddy viscosity (myt/my) max. +// maximum eddy viscosity (myt/my) max. double eddyViscosityLimit = 1.0e10; int monitor_vistmax = 0; -//----------------------------------------------------------------------- -# LES Parameter # -//----------------------------------------------------------------------- +#************************************************************************ +# LES Parameter * +#************************************************************************ // iLES: Create LESSolver or not. -// = 1 - Create LESSolver; -// != 1 - not. +// = 1 -- Create LESSolver; +// != 1 -- not. // amplitudeofDisturb: Amplitude of adding disturb. // disturbstep: Unsteady time step or steady iteration of adding random disturb. // iterdisturb: Add random disturb in every sub-iter or only first sub-iter. -// = 0 - in only first sub-iter; -// != 0 - in every sub-iter. +// = 0 -- in only first sub-iter; +// != 0 -- in every sub-iter. // ipraddisturb: Add density and pressure disturb or not. // ibodyforce: Add body force in source flux of NS equations or not. -// = 0 - not; -// != 0 - Add body force. +// = 0 -- not; +// != 0 -- Add body force. // bodyforce: Body force in source flux of NS equations or not. // utau: friction velocity, using in DNSDisturb. // sgsmodel: subgrid scale model. @@ -820,23 +841,22 @@ int monitor_vistmax = 0; // = "dsmCom"; // = "wale"; // = "sigma". -// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak); -// = 2 - pow(deltai * deltaj *deltak, 1/3); -// = 3 - Devloped by Scotti. -// wallDampingFunctionType: = 0 - no wall function; -// = 1 - van Driest; -// = 2 - developed by Dr. Deng Xiaobing; -// = 3 - developed by Piomelli. +// deltaFunctionType: = 1 -- MAX(deltai, deltaj, deltak); +// = 2 -- pow(deltai * deltaj *deltak, 1/3); +// = 3 -- Devloped by Scotti. +// wallDampingFunctionType: = 0 -- no wall function; +// = 1 -- van Driest; +// = 2 -- developed by Dr. Deng Xiaobing; +// = 3 -- developed by Piomelli. // turbViscousCutType: turbulent viscosity cut type. -// = 0 - mu_total = mut + mul; -// = 1 - mu_total = max(mut-mul,0)+ mul; -// = 2 - mu_total = max(mut ,0)+ mul. +// = 0 -- mu_total = mut + mul; +// = 1 -- mu_total = max(mut-mul, 0) + mul; +// = 2 -- mu_total = max(mut , 0) + mul. // smagConstant: constant of smagorinsky model. // waleConstant: constant of wale model. -// filterDirection[3]: filter variables in i, j, k direction or not. +// filterDirection [3]: filter variables in i, j, k direction or not. // averageDirection[3]: average variables in i, j, k direction or not. // isotropicConstant: constant of isotropic part of SGS stress. - int iLES = 0; string sgsmodel = "smagorinsky"; int deltaFunctionType = 2; @@ -852,19 +872,16 @@ double testFilterScale = 2.0; int averageWidth = 1; int monitorNegativeConstant = 0; -//----------------------------------------------------------------------- -# Other Parameters for Hypersonic Non-equilibrium Gas # -//----------------------------------------------------------------------- +#************************************************************************ +# Other Parameters for Hypersonic Non-equilibrium Gas * +#************************************************************************ // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: // 0 -- gas model is fixed in the codes. // 1 -- gas model is imported from library files. -// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver, -// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver. -// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps. -// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. @@ -875,7 +892,7 @@ int monitorNegativeConstant = 0; // 2 -- Argon. // 3 -- Nitrogen. // nEnergyRecycle: The type of EnergyModel Recycle. -// 0 -- not used . +// 0 -- not used. // 1 -- used. // nDensityModify: The type of densitymodify. // 0 -- not used. @@ -883,26 +900,25 @@ int monitorNegativeConstant = 0; // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. -// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. // 0 -- perfect gas. // 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. -// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. -// the value equals to or is greater than 1, and 3 is for default value. -// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. -// the value equals to or is greater than 1, and 3 is for default value. -// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. -// the value equals to or is greater than 1, and 3 is for default value. -// nSlipBCModel : The computational model of slip boundary conditions. - -// 0 -- no slip. -// 1 -- the conventional Maxwell slip conditions. -// 2 -- the Gokcen slip conditions. -// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. -// 4 -- the Kogan simplified slip conditions. -// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. -// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). -// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. -// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). // nchemsrc: // 0 -- the source terms are not computed. // 1 -- the source terms are computed. @@ -913,148 +929,151 @@ int monitorNegativeConstant = 0; // 1 -- One-temperature model. // 2 -- Two-temperature model. // 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. // nIdealState: whether take all gas species as ideal gas for gas-mixture process. // 0 -- No. -// 1 -- Yes. -// nTEnergyModel: the method to computing temperature energy model. +// 1 -- Yes. // nTEnergyModel: the method to computing temperature energy model. // 0 -- the energy term is computed using the conventional method. // 1 -- the energy term is computed using the polynomial fitting method. // 2 -- the energy term is computed using the piecewise polynomial fitting method. // parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model. // The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value. // catalyticCoef: -// 0.0 -- full non-catalytic wall boundary condition. -// 1.0 -- full catalytic wall boundary condition. -// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient. -// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. -// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. -// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. -// nTemperatureJump : the method to calculate the temperature jump. -// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode. -// 1 -- the general method where the iteration is calculated with the translation-rotation temperature. -// nSurfGradMethod : the method to compute the surface heating ratio. -// 0 -- the gradient of variable is computed with the first-order difference method. -// 1 -- the gradient of variable is computed with the Green-Guass integral method. -// nRapidFlowfield : initialize the flowfield using the rapid engineering method when it is greater than zero. -// nSurfHeatMonitor : To exam the surface heating change or not. 0 is no, 1 is yes. -// nInitPressureStep : the steps to initialize the boundary variables when the rapid method is used. 100 is the default value. -// nDumpCFLNumber : 1 indicates dumping the CFL number to file, 0 denotes no dumping. +// 0.0 -- full non-catalytic wall boundary condition. +// 1.0 -- full catalytic wall boundary condition. +// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// nTemperatureJump: the method to calculate the temperature jump. +// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode. +// 1 -- the general method where the iteration is calculated with the translation-rotation temperature. +// nSurfGradMethod: the method to compute the surface heating ratio. +// 0 -- the gradient of variable is computed with the first-order difference method. +// 1 -- the gradient of variable is computed with the Green-Guass integral method. +// nRapidFlowfield: initialize the flowfield using the rapid engineering method when it is greater than zero. +// nSurfHeatMonitor: To exam the surface heating change or not. 0 is no, 1 is yes. +// nInitPressureStep: the steps to initialize the boundary variables when the rapid method is used. 100 is the default value. +// nDumpCFLNumber: 1 indicates dumping the CFL number to file, 0 denotes no dumping. // sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0]. // sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0]. // sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0]. // velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. -// 1.0 -- proposed by Maxwell. -// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. -// 1.146 -- proposed for an additional "fictitious" velocity slip. - -// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. -// spectrumRadiusCoef: The value is in range of [0.0, 2.0]. -// staticPressureRelaxCorf: The value is in range of [0.1, 1.0]. -// nIsChemicalFreeze : the flag to freeze the chemical reactions. -// 0 -- not freeze, the chemical reaction sources will be calculated. -// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te - -//maxViscous: the maximum of Viscous. -//trTemperatureMin: the minimum value of trTemperature. -//veTemperatureMin: the minimum value of veTemperature. -//densityMin: the minimum value of density. -//tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0]. -// nDebug: cout the Wrong place and abort -// 0 -- not used. -// 1 -- used. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// spectrumRadiusCoef: The value is in range of [0.0, 2.0]. +// staticPressureRelaxCorf: The value is in range of [0.1, 1.0]. +// nIsChemicalFreeze: the flag to freeze the chemical reactions. +// 0 -- not freeze, the chemical reaction sources will be calculated. +// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated. +// veTemperatureMin: The minimum of Tv and Te. +// maxViscous: the maximum of Viscous. +// trTemperatureMin: the minimum value of trTemperature. +// veTemperatureMin: the minimum value of veTemperature. +// densityMin: the minimum value of density. +// tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0]. +// nDebug: cout the Wrong place and abort +// 0 -- not used. +// 1 -- used. // nSpeciesLimit: limitter of gas species -// 0 -- not used. -// 1 -- used. -// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction -// 0 -- method 0. -// 1 -- method 1. -// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid -// 0 -- not used. -// 1 -- used. -// nViscosityPeModified: Pe Modified for ViscosityCoef -// 0 -- not used. -// 1 -- used. -// nChemcalSourceModified: Modified on ChemcalSource -// 0 -- not used. -// 1 -- used. -// nChemcalSourceEsMethod: Modified on ChemcalSource -// 0 -- approximation algorithm 1 (Ori.) -// 1 -- approximation algorithm 2 (New) - +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid. +// 0 -- not used. +// 1 -- used. +// nViscosityPeModified: Pe Modified for ViscosityCoef. +// 0 -- not used. +// 1 -- used. +// nChemcalSourceModified: Modified on ChemcalSource. +// 0 -- not used. +// 1 -- used. +// nChemcalSourceEsMethod: Modified on ChemcalSource. +// 0 -- approximation algorithm 1 (Ori). +// 1 -- approximation algorithm 2 (New). // nMaxStepTemperature: the iterative steps of temperature. - -// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs -// 0 -- not used -// 1 -- used - -// nDiagonalModified: Modified on Diagonal -// 0 -- not used -// 1 -- Ori. -// 2 -- new - -//nGradPrimtiveMethod: -// 0 -- Ori. -// 1 -- new +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. // nAblation: -// 0 -- The wall ablation is not computed. -// 1 -- The wall ablation is computed. +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. // isInjection: -// 0 -- The injection velocity of ablation wall is not computed. -// 1 -- The injection velocity of ablation wall is computed. +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. // nViscosityModel: -// 0 -- Blottner fitting method(N89). -// 1 -- Gupta fitting method(N90). +// 0 -- Blottner fitting method(N89). +// 1 -- Gupta fitting method(N90). // nContinueModel: The new continue model can switch different computation model. -// 0 -- Not use the new continue model. -// 1 -- use the new continue model. +// 0 -- Not use the new continue model. +// 1 -- use the new continue model. // nSutherland: -// 0 -- stands for selecting the Blotter curve fits mode. -// 1 -- stands for Sutherland relation. +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. // gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11". -// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. -// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. -// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. -// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. -// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. -// "Gas-Mixture" -- indicates the process of mixing gas without reacting. -// for struct solver mixing two speciesSpeciesA, SpeciesB. -// for unstruct solver mixing multi-speciesO2 NO CO CO2 H2 N2 Air CH4. -// For self-definition model, the gasfile is used to indicate the file path of the new gas model. +// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. +// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. +// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "Gas-Mixture" -- indicates the process of mixing gas without reacting. +// for struct solver mixing two species��SpeciesA, SpeciesB��. +// for unstruct solver mixing multi-species��O2 NO CO CO2 H2 N2 Air CH4��. +// For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. // ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes. -// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation. -// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation. -// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation. -// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory. -// 0 -- no, -// 1 -- yes. +// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation. +// nIterSecondStep: the maximum number of iteration in the second step for the self-adaptive calculation. +// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation. +// nEnergyAssembly: the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory. +// 0 -- no, +// 1 -- yes. // nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model. -// 0 -- the density. -// 1 -- the translation temperature. -// 2 -- the vibration temperature. -// 3 -- the electron temperature. -// 4 -- the pressure. -// 5 -- the mass fraction of oxygen. -// 6 -- the mass fraction of nitrogen. +// 0 -- the density. +// 1 -- the translation temperature. +// 2 -- the vibration temperature. +// 3 -- the electron temperature. +// 4 -- the pressure. +// 5 -- the mass fraction of oxygen. +// 6 -- the mass fraction of nitrogen. // firstStepError : the residual error of the first step iteration for the self-adaptive calculation. // secondStepError : the residual error of the second step iteration for the self-adaptive calculation. // thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. -// useHyflowSetting : Setting for HyFLOW GUI. -// 0 -- PHengLEI -// 1 -- HyFLOW -// nProtectData : Use the continuation file data protection mechanism. -// 0 -- no -// 1 -- yes - +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. int dg_high_order = 0; int iapplication = 0; int isAdaptiveSolver = 0; -int nm = 5; +int nm = 5; int nEquilibriumGas = 0; -int nPCWCycleStep = 3; -int nRETCycleStep = 3; -int nSLIPCycleStep= 3; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; int nIterFirstStep = 1000; int nIterSecondStep= 2000; int nIterThirdStep = 2000; @@ -1065,17 +1084,17 @@ double secondStepError = 0.001; double thirdStepError = 0.001; double predictCFLError = 0.1; -double refGama = 1.4; -double prl = 0.72; -double prt = 0.90; -double sc_l = 0.5; -double sc_t = 0.5; +double refGama = 1.4; +double prl = 0.72; +double prt = 0.90; +double sc_l = 0.5; +double sc_t = 0.5; -int nGasModel = 0; -int nchem = 0; -int nchemsrc = 1; -int nchemrad = 1; -int ntmodel = 1; +int nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; int nIdealState = 0; int nEnergyRecycle = 1; @@ -1099,12 +1118,12 @@ double sigmaTemperature = 1.0; double sigmaMassFraction = 1.0; double velocitySlipCorrectConstant = 1.0; -double chemicalRelaxCorf = 1.0; +double chemicalRelaxCorf = 1.0; double chemicalSpectrumRadiusCoef = 1.0; double viscousSpectrumRadiusCoef = 1.5; double inviscidSpectrumRadiusCoef = 1.5; -double spectrumRadiusCoef = 0.5; -double staticPressureRelaxCorf = 0.2; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; double maxViscous = 10000.0; double trTemperatureMin = 10.0; @@ -1114,31 +1133,35 @@ double densityMin = 1.0e-8; double densityMinFactor = 0.1; double tAdjustmentFactor = 10.0; double iniSpeedCoef = 1.0; +int iniSpeedMode = 0; -int nDebug = 0; -int nSpeciesLimit = 1; -int nTurblenceForChemical = 0; -int nViscosityFluxSublevelModified = 1; -int nViscosityPeModified = 0; -int nChemcalSourceModified = 2; -int nChemcalSourceEsMethod = 1; -int nMaxStepTemperature = 5; -int veTemperatureMinModified = 1; -int nDiagonalModified = 0; -int nGradPrimtiveMethod = 1; -int nInviscidFluxModify = 1; -int nQlLimitMethod = 2; -int nSpeciesForWallMethod = 1; -int nDensityForWallMethod = 0; +int nDebug = 0; +int nSpeciesLimit = 1; +int nTurblenceForChemical = 0; +int nViscosityFluxSublevelModified = 1; +int nViscosityPeModified = 0; +int nChemcalSourceModified = 2; +int nChemcalSourceEsMethod = 1; +int nMaxStepTemperature = 5; +int veTemperatureMinModified = 1; +int nDiagonalModified = 0; +int nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; -int nProtectData = 0; -int useHyflowSetting = 0; -int nAblation = 0; -int isInjection = 0; -int nViscosityModel = 0; -int nMarsModel = 0; -string gasfile = "DK5"; -//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; string speciesName = "O, O2, NO, N, N2"; string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; @@ -1152,16 +1175,16 @@ string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; //string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; //string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; -//string gasfile = "Pa"; +//string gasfile = "Pa"; //string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0"; -//string gasfile = "Combustion-12"; +//string gasfile = "Combustion-12"; //string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; //string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; //string gasfile = "Gas-Mixture"; -//string speciesName ="SpeciesA, SpeciesB"; +//string speciesName = "SpeciesA, SpeciesB"; //string initMassFraction = "1.0, 0.0"; int nSutherland = 0; double gamaSpeciesA = 1.4; @@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0; //string speciesName = "O2, N2"; //string initMassFraction = "1.0, 0.0"; +int nFraction = 0; int nContinueModel = 0; int nChemicalFlowStep = 0; int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; ######################################################################### // Multi-Grid parameters. @@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0; // 1 -- zero order. // 2 -- first-order. (default) // mgCorrectionLimit: Multi-grid correction limit. - int nMGLevel = 1; int MGCoarsestIteration = 1; int MGPreIteration = 1; @@ -1218,20 +1248,20 @@ int ismooth_turb = 0; int SAProductType = 2; // ----------------- Overset Grid parameter ----------------------------- -int codeOfDigHoles = 1; -int codeOfTurbulentModel = 0; -string masterFileName = "./grid/searchFile.inp"; -string holeBasicFileName = "./grid/holeBasicFile.inp"; -string holeFullFileName = "./grid/holeFullFile.dat"; -string linkFileName = "./grid/topology.dat"; -string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; +int codeOfDigHoles = 1; +int codeOfTurbulentModel = 0; +string masterFileName = "./grid/searchFile.inp"; +string holeBasicFileName = "./grid/holeBasicFile.inp"; +string holeFullFileName = "./grid/holeFullFile.dat"; +string linkFileName = "./grid/topology.dat"; +string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; -######################################################################### -# High Order Struct Solver # -######################################################################### +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ // isFVMOrFDM: -// 0 -- NSSolverStruct using Finite Volume Method. -// 1 -- NSSolverStruct using Finite Differ Method. +// 0 -- NSSolverStruct using Finite Volume Method. +// 1 -- NSSolverStruct using Finite Differ Method. // SolverStructOrder: Spatial discretisation order of NS equations with struct grid. // <= 2 -- finite volume method. // >= 3 -- finite difference order. (to be completed) @@ -1273,30 +1303,48 @@ int allReduceStep = 1; // codeOfOversetGrid: Overlapping(overset) grid or not. // 0 -- NON-overlapping grid. // 1 -- Overlapping grid. -// oversetInterpolationMethod: the method of overset interpolation while field simulation +// oversetInterpolationMethod: the method of overset interpolation while field simulation. // 0 -- set the acceptor cell value by donor cell value. // 1 -- set the acceptor cell value by distance weight of donor cell value. - -int codeOfOversetGrid = 0; -int oversetInterpolationMethod = 0; -int readOversetFileOrNot = 0; -int symetryOrNot = 0; -int readInAuxiliaryInnerGrid = 0; -int readInAuxiliaryOuterGrid = 0; -int readInSklFileOrNot = 0; -string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; -string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; -string auxiliaryInnerGrid2 = ""; -string oversetGridFileName = "./grid/iblank.ovs"; -double walldistMainZone = 1.0 -double toleranceForOversetSearch = 1.0e-3; -double toleranceForOversetBox = 1.0e-3; -int twoOrderInterpolationOrNot = 0; -int keyEnlargeOfActiveNodes = 0; -int outTecplotOverset = 0; -int outPutOversetVisualization = 0; - -int numberOfMovingBodies = 2; +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.ovs"; +double walldistMainZone = 1.0 +double toleranceForOversetSearch = 1.0e-3; +double toleranceForOversetBox = 1.0e-3; +int twoOrderInterpolationOrNot = 0; +int keyEnlargeOfActiveNodes = 0; +int outTecplotOverset = 0; +int outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; // ----------------- ALE configuration ------------------------------ int codeOfAleModel = 0; @@ -1306,36 +1354,42 @@ double referenceLength = 1.0; double referenceVelocity = 1.0; double referenceDensity = 1.0; -int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd; -int strategyForGCLSource = 0; //0-present; 1-Ahn; +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. -//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. int methodForKineticEquation = 0; double relaxParameterOfKinetic = 1.0; -######################################################################### -# motive information # -######################################################################### +#************************************************************************ +# motive information * +#************************************************************************ int numberOfMovingBodies = 1; ############################## body0 ############################## -//mass of parts -double mass_0 = 1.0; -//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz -double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; -//initial six DOF position information of parts. xc yc zc -double massCenter_0[] = 0.0 , 0.0, 0.0; -//initial six DOF position information of parts. angleX angleY angleZ -double attitudeAngle_0[] = 0.0 , 0.0, 0.0; -//initial six DOF move information of parts. vc vy vz -double massCenterVelocity_0[] = 0.0, 0.0, 0.0; -//initial six DOF move information of parts. omigX omigY omigZ -double angularVelocity_0[] = 0.0, 0.0, 0.0; -//the object that the parts belong to. -int fartherIndex_0 = -1; -//the assembly position of the parts. xc yc zc angleX angleY angleZ -double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0; -//the move pattern of the parts. +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. // -1 given motion partten. // 0 still. // 1 six DOF motion. @@ -1346,51 +1400,68 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 // 14 forced pitch motion. // 15 forced yaw motion. // 16 forced roll motion. -int RBDMethod_0 = 0; -double amplitude_0 = 0.0; -double reduceFrequency_0 = 0.0; -//direction of rotation +int RBDMethod_0 = 0; +double amplitude_0 = 0.0; +double reduceFrequency_0 = 0.0; +// direction of rotation. // 1 -- clockwise from the point of view along the positive x axis. // -1 -- anticlockwise from the point of view along the positive x axis. -int direction_0 = -1; -double rotateFrequency_0 = 0.0; -//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; -//additional force (system axis) fX fY fZ -double addedForce_0[] = 0.0 ,0.0 ,0.0 ; -//additional moment of Force (system axis) mX mY mZ -double addedMoment_0[] = 0.0 ,0.0 ,0.0 ; -//the deformation method of the parts. -int morphing_0 = 0; - -// post indentify -int integralOrder = 4; +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; +// post indentify. +int integralOrder = 4; // ---------------- ATP read -------------------------------------------- -//@int inflowParaType = 0; +//@int inflowParaType = 0; //@double refReNumber = 6.5e6; //@double refDimensionalTemperature = 288.15; //@double freestream_vibration_temperature = 300.00; -//@double refDimensionalPressure = 0; -//@double height = 0; -//@int nsubsonicInlet = 0; -//@int nsubsonicOutlet = 0; -//@string inLetFileName = "./bin/subsonicInlet.hypara"; -//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; //@double refDimensionalVelocity = 0; //@double refDimensionalDensity = 0; - -######################################################################### -# Old Parameter # -######################################################################### +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ int isPlotVolumeField = 0; +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; -######################################################################### -# Incompressible Parameter # -######################################################################### +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ int isSolveEnergyEquation = 0; int isSolveTurbEquation = 0; -int isSolveSpeciesEquation = 0; - +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/L04_ThreeD_Spoiler_BGK_MPI_8CPU/bin/input.txt b/L04_ThreeD_Spoiler_BGK_MPI_8CPU/bin/input.txt new file mode 100644 index 0000000..b6ed269 --- /dev/null +++ b/L04_ThreeD_Spoiler_BGK_MPI_8CPU/bin/input.txt @@ -0,0 +1,35 @@ +0 ！MRT set 1, BGK set 0 +0 continue.plt ！CONTI, resume :1 , new 0 //follows input datafile name //use ASCII文件 continue.plt +0 ！LES yes: 1 , no: 0 +1 mesh_3d.dat ！GEO read complex geo? yes:1, no:0 //follows input datafile name +0 ! MB multiblock LBM? yes:1, no:0 +0 2e-3 !CONV using converge criterion? yes:1, no:0 +100 ！NX +300 ! NY +100 ! NZ +1 ！ NX2 +1 ！ NY2 +1 ! NZ2 +0 ! LowX +0 ! LowY +0 ! LowZ +2 ! x_np +2 ! y_np +2 ! z_np +400 ! framerate +2000 ！total steps to terminate +1.0 ! density +0.56 ！ tau +(0.0,0.0,0.0) ！ Volumetric force +D3Q19 ! velocity set +3Dspoiler ! boundary condition +! note: in the following, boundary types: periodic,velocity, pressure +! are allowed. if "velocity" is applied, please strictly follow the format "velocity (%lf, %lf, %lf)". +velocity (0.00, 0.1, 0.0) ！xmin face +velocity (0.00, 0.1, 0.0) ！xmax face +velocity (0.00, 0.1, 0.0) ！ymin face +pressure 1.0 ！ymax face, +velocity (0.00, 0.1, 0.0) ！zmin face +velocity (0.00, 0.1, 0.0) ！zmax face +-------------------！ initial velocity field +(0.0, 0.1, 0.0) \ No newline at end of file diff --git a/L04_ThreeD_Spoiler_BGK_MPI_8CPU/bin/key.hypara b/L04_ThreeD_Spoiler_BGK_MPI_8CPU/bin/key.hypara new file mode 100644 index 0000000..1a572c7 --- /dev/null +++ b/L04_ThreeD_Spoiler_BGK_MPI_8CPU/bin/key.hypara @@ -0,0 +1,55 @@ +string title = "PHengLEI Main Parameter Control File"; + +// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE. +string defaultParaFile = "./bin/cfd_para.hypara"; + +// ndim: Dimensional of the grid, 2 or 3. +// nparafile: the number of parameter files. +// nsimutask: simulation task type. +// 0 -- CFD Solver of NS or Turbulation. +// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc. +// Grid conversion: from other format to PHengLEI format (.fts). +// Grid reconstruction: such as grid adaptation. +// Grid merging: merge two blocks into one block. +// Grid repairing: repair the original grid in order to remove the negative volume cells. +// 2 -- Wall distance computation for turb-solver. +// 3 -- Grid partition. +int ndim = 3; +int nparafile = 1; + +//int nsimutask = 0; +//string parafilename = "./bin/cfd_para_subsonic.hypara"; +//string parafilename = "./bin/cfd_para_transonic.hypara"; +//string parafilename = "./bin/cfd_para_supersonic.hypara"; +//string parafilename = "./bin/cfd_para_hypersonic.hypara"; +//string parafilename = "./bin/cfd_para_incompressible.hypara"; + +//int nsimutask = 1; +//string parafilename = "./bin/grid_para.hypara"; + +//int nsimutask = 2; +//string parafilename = "./bin/cfd_para.hypara"; + +//int nsimutask = 3; +//string parafilename = "./bin/partition.hypara"; + +//int nsimutask = 1; +//string parafilename = "./bin/grid_deform_para.hypara"; + +//int nsimutask = 1; +//string parafilename = "./bin/grid_refine_para.hypara"; + +int nsimutask = 13; +string parafilename = "./bin/cfd_para.hypara"; + +//int nsimutask = 14; +//string parafilename = "./bin/integrative_solver.hypara"; + +//int nsimutask = 99; +//string parafilename = "./bin/post_processing.hypara"; + +// ---------------- Advanced Parameters, DO NOT care it ---------------- +int numberOfGridProcessor = 0; +// ATP read +//@string parafilename1 = "" +//@string parafilename2 = ""; diff --git a/L04_ThreeD_Spoiler_BGK_MPI_8CPU/mesh_3d.dat b/L04_ThreeD_Spoiler_BGK_MPI_8CPU/mesh_3d.dat new file mode 100644 index 0000000..d1ce06f --- 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637 + 640 576 637 + 576 640 643 + 645 639 641 + 633 639 645 + 645 635 633 + 645 643 635 + 646 641 642 + 645 641 646 + 646 642 644 + 643 645 646 + 646 576 643 + 646 644 576 diff --git a/L05_TwoD_Cavity_BGK_OMP_1CPU/bin/cfd_para.hypara b/L05_TwoD_Cavity_BGK_OMP_1CPU/bin/cfd_para.hypara new file mode 100644 index 0000000..f903a5a --- /dev/null +++ b/L05_TwoD_Cavity_BGK_OMP_1CPU/bin/cfd_para.hypara @@ -0,0 +1,1467 @@ +//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ +// PPPPP H H EEEEE N N GGGGG L EEEEE III + +// P P H H E NN N G L E I + +// PPPPP HHHHH EEEEE N N N G GG L EEEEE I + +// P H H E N N N G G L E I + +// P H H EEEEE N N GGGGG LLLLL EEEEE III + +//------------------------------------------------------------------------+ +// Platform for Hybrid Engineering Simulation of Flows + +// China Aerodynamics Research and Development Center + +// (C) Copyright, Since 2010 + +// PHengLEI 2212 + +//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ +########################################################################### +# Default parameters for Grid conversion # +########################################################################### +// gridtype: Grid type for generation, conversion, reconstruction, merging. +// 0 -- Unstructured grid. +// 1 -- Structured grid. +// 2 -- Hybrid grid, include both of unstructured and structured grid. +// gridobj: Task type of grid treatment. +// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc. +// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS. +// 2 -- Grid refinement. +// 3 -- Grid merging, merge two blocks into one block. +// 4 -- Grid deformation, achieve unstructured grid deformation. +// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells. +// 6 -- Grid mirroring, mirror a symmetry grid to whole grid. +// 7 -- Grid type change, convert structured grid to unstructured grid. +// multiblock: Multi-block grid or not, only for structured grid conversion. +// 0 -- Not. +// 1 -- Yes. +// iadapt: Adaptation number for unstructure grid. +// SymmetryFaceVector: The vector of symmetry face. +// 0 -- X axis. +// 1 -- Y axis. +// 2 -- Z axis. +// gridReorder: Reorder cell and face of grid or not, only for 3D unstructured grid conversion, +// which is CGNS type. +// 0 -- Not. +// 1 -- Yes. +// faceReorderMethod: the reorder method face of unstructured grid. +// 0 -- BSFCELLFACEORG. +// 1 -- BSFCELLFACELEFT. +// 2 -- BSFCELLFACERIGHT. +int gridtype = 0; +int gridobj = 1; +int multiblock = 0; +int iadapt = 0; +int SymmetryFaceVector = 1; +int gridReorder = 0; +int faceReorderMethod = 0; + +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; + +// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". +// 0 -- Interface. (default) +// 1 -- Physical boundary condition, used in Hybrid solver. +int omit_no_bound_bc = 0; +int omitRepeatInterface = 1; + +//----------------------------------------------------------------------- +# Grid data type # +//----------------------------------------------------------------------- +// from_gtype/to_gtype: Type of grid data type in grid conversion process. +// -1 -- MULTI_TYPE. +// 1 -- PHengLEI, *.fts. +// 2 -- CGNS, *.cgns. +// 3 -- Plot3D type of structured grid, *.dat/*.grd. +// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. +// 5 -- Fluent, *.cas/*.msh. +// 6 -- Ustar, mgrid.in. +// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. +// 8 -- GMSH, *.msh. +// 9 -- Gridgen type of structured grid, *.dat/*.grd. +// dumpOldGrid: If dump out the old grid file. +// 0 -- Not. (default) +// 1 -- Yes. +int from_gtype = 2; +int to_gtype = 1; +int dumpOldGrid = 0; + +//----------------------------------------------------------------------- +# File path # +//----------------------------------------------------------------------- +// from_gfile: path of original data file for unstructure grid convert from. +// out_gfile: path of target file for grid convert to, *.fts type of file usually. +int numberOfGridFile = 1; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; + +// ----------------- some advanced choices ------------------------------ +// iunsteady: The Grid is for unsteady simulation or not. +int iunsteady = 0; + +// fileformat: Ustar Grid file format. +// 0 -- BINARY. +// 1 -- ASCII. +int fileformat = 0; + +// Parameters for hybrid solver. +// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type. +// mixgrid_str: path of structure grid file for hybrid solver, *.fts type. +string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; +string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; + +// Some parameters for structured overlapping grid. +int codeOfDigHoles = 1; +string holeBasicFileName = "./oversetGridView/holeBasicFile.inp"; +string holeFullFileName = "./oversetGridView/holeFullFile.dat"; +string linkFileName = "./oversetGridView/topology.dat"; +string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; + +// ----------------- Grid Refine Parameters ----------------------------- +// anisoRefine: If refine grid by anisoRefine type. +// 0 -- Not. (default) +// 1 -- Yes. +// geometryUnit: Geometry unit. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. +// exclusiveCase: Parallel projection exclusive case. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. +// projectOrgPoint: If the original wall points need to be projected or not. +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; +int exclusiveCase = 0; +int projectOrgPoint = 0; +string geometryFileName = "./grid/jsm.igs"; + +// ----------------- Grid Deform Parameters ----------------------------- +// deformationMethod: Grid Deform. +// 1 -- SPRING. +// 2 -- RBF. +// stationalGridFile: Original grid file. +// visualFileName : The visualization file path of deform grid. +// nDeformStep : The max deform step. +// flapAngle : The max flap angle. +// rotatePostionZ : Rotate postion. +// rotatePostionY : Rotate postion. +// gridSlice : If dump slice grid. +// sliceAxis : Grid slice axis. +// slicePosition : Grid slice position. +int nDeformStep = 40; +double flapAngle = 10.0; +double rotatePostionZ = 4.00003; +double rotatePostionY = 3.05; + +int deformationMethod = 2; +string stationalGridFile = "./grid/Segment2Brid.fts"; +string visualFileName = "./results/deformedGrid.dat" + +int gridSlice = 1; +int sliceAxis = 1; +double slicePosition = 13; + +// ----------------- RBF Parameters ------------------------------------- +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. +int numberOfReferenceCP = 40; +double influencePara = 25.0; + +// ----------------- Periodic Parameters -------------------------------- +// Notice: Rotational periodicity only support rotation along the X axis! +// periodicType: Which periodic boundary is used. +// 0 -- without Periodic Boundary. +// 1 -- Translational periodicity. +// 2 -- Rotational periodicity. +// translationLength[]: The relative distance between two periodic face + which only support one direction. +// rotationAngle: The relative angle between two periodic face. + which is recorded in degrees. +int periodicType = 0; +double translationLength[] = [0.0, 0.0, 0.0]; +double rotationAngle = 0.0; + +######################################################################### +# Default parameters for Partition # +######################################################################### +// pgridtype: The grid type. +// 0 -- unstruct grid. +// 1 -- struct grid. +// 2 -- refine structured grid. +// maxproc: The number of partition zones that want to be divided into. +// numberOfMultifile: The number of partition grid files that want to be dumped out. +int pgridtype = 0; +int maxproc = 4; +int numberOfMultifile = 1; + +// traceMark: Trace mark or not, only for structured grid partition. +// 0 -- Not. +// 1 -- Yes. +// blockIndexOfMark: the block index of mark, only for structured grid partition. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. +int traceMark = 0; +int blockIndexOfMark = 0; +int cellIndexOfMark[] = [185, 30, 1]; + +// parallelStrategy: +// 0 -- each zone is assigned to the one that defined in grid partition procedure. +// 1 -- random assigned for each zone or by some else ways. +int parallelStrategy = 1; + +//----------------------------------------------------------------------- +# File path # +//----------------------------------------------------------------------- +// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). +// partition_grid_file: Target partition grid file(PHengLEI type, *.fts). +string original_grid_file = "./grid/sphere_mixed.fts"; +string partition_grid_file = "./grid/sphere_mixed__4.fts"; + +// ------------------ Sompe advanced parameters ------------------------- +// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". +// 0 -- Interface. (default) +// 1 -- Physical boundary condition, used in Hybrid solver. +// npartmethod: Method of interface reconstruction, default is 1. +// parallelPartitionMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition. +// 1 -- Using ParMetis for homogeneous MPI. +// 2 -- Using Metis for homogeneous MPI. +// 3 -- using METIS partition for homogeneous OpenMP. +// parmetisBalance: Used to specify the imbalance tolerance. +// 1 -- perfect balance. +// maxproc -- perfect imbalance. +// 1.05 -- recommended. +int omit_no_bound_bc = 0; +int npartmethod = 1; +int parallelPartitionMethod = 2; +double parmetisBalance = 1.05; + +// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. +// 1 -- single level. +// 2 -- 2 level. +// N -- N level, ..., et al. +int numberOfMultigrid = 1; + +######################################################################### +# Default parameters for CFD simulation # +######################################################################### +// maxSimuStep: The max simulation step, don't care simulation is restart or not. +// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. +// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. +// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved. +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; +int intervalStepSample = 1000; +int intervalStepForce = 100; +int intervalStepRes = 10; + +// compressible: +// 0 -- incompressible flow. +// 1 -- compressible flow. (default) +int compressible = 1; + +// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. +// 0 -- no precondition process. (default, mach > 0.3) +// 1 -- carry out precondition process. (mach number <= 0.3) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + +//----------------------------------------------------------------------- +# CFD Control Parameter # +//----------------------------------------------------------------------- +// refMachNumber: Mach number. +// attackd: Angle of attack. +// angleSlide: Angle of sideslip. +// inflowParaType: The type of inflow parameters. +// 0 -- the nondimensional conditions. +// 1 -- the flight conditions. +// 2 -- the experiment conditions. +// 3 -- the subsonic boundary conditions. (Useless!) +// 4 -- the condition that the velocity, temperature and density are given. +// 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. +// refReNumber: Reynolds number, which is based unit length, unit of 1/m. +// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. +// freestream_vibration_temperature: Dimensional freestream vibration temperature. +// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition. +// height: Fly height, unit of km. +// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition. +// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter. Common dimensions like: +// 1 dm = 0.1 m. +// 1 cm = 0.01 m. +// 1 mm = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. +// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit. +// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit. +// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary +// condition is radiation equilibrium temperature, and 0.8 is the default value. +// refMolecularWeight: the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on. +int directionMethod = 0; +double refMachNumber = 0.73; +double attackd = 2.79; +double angleSlide = 0.00; +int flowInitMethod = 0; + +int inflowParaType = 0; +double refReNumber = 6.5e6; +double refDimensionalTemperature = 288.15; +double freestream_vibration_temperature = 300.00; + +//int inflowParaType = 1; +//double height = 0.001; + +//int inflowParaType = 2; +//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2). +//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)). + +// The velocity, temperature and density are fixed. +//int inflowParaType = 4; +//double refDimensionalVelocity = 1000.0; +//double refDimensionalDensity = 1.0e3; + +// The velocity, temperature and pressure are fixed. +//int inflowParaType = 5; +//double refDimensionalVelocity = 1000.0; +//double refDimensionalPressure = 1.0e5; + +// The MachNumber, temperature and pressure are fixed. +//int inflowParaType = 6; +//double refDimensionalTemperature = 293.0; +//double refDimensionalPressure = 8886.06; + +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + +double wallTemperature = -1.0; + +double radiationCoef = 0.8; +double gridScaleFactor = 1.0; +double gridTranslationVector[] = [0.0, 0.0, 0.0]; + +int numberOfAerodynamicForceComponents = 1; +double forceReferenceLengthSpanWise = 1.0; // unit of meter. +double forceReferenceLength = 1.0; // unit of meter. +double forceReferenceArea = 1.0; // unit of meter^2. +double TorqueRefX = 0.0; // unit of meter. +double TorqueRefY = 0.0; // unit of meter. +double TorqueRefZ = 0.0; // unit of meter. +double knudsenLength = 1.0; // unit of meter. +double refMolecularWeight = 28.9644; // unit of g/mol. + +//----------------------------------------------------------------------- +# Spatial Discretisation # +//----------------------------------------------------------------------- +#************************************************************************ +# Struct Solver * +#************************************************************************ +// inviscidSchemeName: Spatial discretisation scheme of struct grid. +// Using this when solve structered grid or hybrid. +// -- "vanleer", "steger", "hlle", "lax_f", +// -- "roe", "modified_roe", +// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+". +// isWennScheme: If using WENN Scheme of struct grid. +// 0 -- NO. (default) +// 1 -- Yes. +// str_limiter_name: Limiter of struct grid. +// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth", +// -- "nolim", no limiter, +// -- "vanalbada_clz", clz supersonic version, +// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3". +string inviscidSchemeName = "roe"; +int isWennScheme = 0; +string str_limiter_name = "vanalbada"; + +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ +// viscousType: Viscous model. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. +// viscousName: Laminar or tubulent model. +// -- "0eq-bl". +// -- "1eq-sa". +// -- "2eq-kw-menter-sst". +// -- "2eq-kw-menter-bsl". +// -- "2eq-kw-wilcox-1988". +// -- "2eq-kw-wilcox-1998". +// -- "2eq-kw-kok-tnt". +// -- "2eq-kw-wilcox-2006". +// -- "easm-kw-2003". +// -- "easm-kw-2005". +// DESType: Type of DES. +// 0 -- RANS. (default) +// 1 -- DES. +// 2 -- DDES. +// 3 -- IDDES. +// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. +// Using this when solve Unstructered grid or hybrid. +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", +// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". +// uns_limiter_name: Limiter of Unstruct grid. +// -- "barth", "vencat", "vanleer", "minmod", +// -- "vanalbada", "smooth", "nnd", "lpz", "1st", +// -- "nolim", no limiter. +// uns_vis_name: Discretisation method of viscous term. +// -- "std", "test", "aver", "new1", "new2". +// gradientName: Gradient reconstruction method. +// -- "default", "ggcell", "ggnode", "lsq". +// ivencat: Variation of vencat limiter. +// 0 -- org method, it is independent of grid scale. +// 1 -- new method, it is dependent of grid scale. +// 4 -- Ustar limiter model, without grid size unitary. +// 7 -- default used. +// venkatCoeff: Cofficient of vencat, when using vencat limter. +// limitVariables: Limit model (It is useful only if limitVector is 0). +// 0 -- limit only for pressure and denstiny, then get the min value. +// 1 -- limit for every variables, then get the min value. +// limitVector: +// 0 -- Each variable use the same limiter coefficient. +// 1 -- Each variable use the respective limiter coefficients. +// reconmeth: +// 0 -- When reconstruct face value, Q+, Q- use respective limiter coefficients. +// 1 -- Q+, Q- use the min limiter coefficients of left and right cell. +// skewnessAngle: The skewness angle of grid cells. +// roeEntropyFixMethod: Entropy fix (correction) method. +// 1 -- direct fix, which limits the minimum eigenvalue directly. +// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver. +// 3 -- Harten type, which is default used. +// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0. +// It is used to scale the default Roe entropy fix coefficients. +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. + +//int viscousType = 0; +//string viscousName = "Euler"; + +//int viscousType = 1; +//string viscousName = "laminar"; + +int viscousType = 3; +string viscousName = "1eq-sa"; + +//int viscousType = 4; +//string viscousName = "2eq-kw-menter-sst"; + +int DESType = 0; + +string uns_scheme_name = "roe"; +string uns_limiter_name = "vencat"; +string uns_vis_name = "test"; +string gradientName = "ggnode"; + +int ivencat = 7; +double venkatCoeff = 5.0; +int reconmeth = 1; +int limitVariables = 0; +int limitVector = 0; +double skewnessAngle = 60.0; + +int roeEntropyFixMethod = 3; +double roeEntropyScale = 1.0; + +double AusmpwPlusLimiter = 1.0; + +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ +// iunsteady: Steady or unsteady. +// 0 -- steady. +// 1 -- unsteay. +// physicalTimeStep: The nondimensional physical time step. +// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes. +// ifStaticsFlowField: Statistical variables for unsteady simulation. +// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation. +// startStatisticStep: Outer step when start statistics. +// when the value is larger than "maxSimuStep", it is useless. +// statisticalTimePeriod: Used as time period of statistic analysis. +// when the value is negative, time period is treated as infinite. +// statisticMethod: Statistic reynolds stress method. +// 0 -- tau = - ^2 +// 1 -- tau = +// min_sub_iter: The min sub iteration of unsteady simulation. +// max_sub_iter: The max sub iteration of unsteady simulation. +// tol_sub_iter: The tolerance of sub iteration of unsteady simulation. +// tscheme: Temporal Discretisation method. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. +// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. +// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. +// CFLStart: Started cfl number. +// CFLEnd: End cfl number. +// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. +// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) +// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. +// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. +// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS. +// ifLocalTimeStep: Time step method. +// 0 --Local. +// 1 --Global. +// isUseLocalCFL: use variable number of CFL or not. +// 0 -- global unified CFL number. +// 1 -- local CFL number. +// isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no. +// visl_min: Minimum value of laminar viscosity coefficient. +// turbCFLScale: Turbulence model cfl number factor. +// codeOfAleModel: Arbitrary Lagrangian-Eulerian method. +// 0 -- no ALE method. +// 1 -- ALE method for non-moving grids. +// 2 -- ALE method for moving grids. +// 3 -- ALE method for deforming grids. +// wallFunctionType: The type of wall function to implement. +// 0 -- no wall function. (default) +// 1 -- standard wall function. +// 2 -- Pab3D wall function. +// RKStage: The number of Runge-Kutta step. +// lamda: Cofficient of Runge-Kutta step. +int iunsteady = 0; +double physicalTimeStep = 0.01; +double physicalTimeStepDimensional = -0.001; +int ifStartFromSteadyResults = 0; +int ifStaticsFlowField = 0; +int ifStaticsReynoldsStress = 0; +int startStatisticStep = 800000; +double statisticalTimePeriod = -1.0; +int statisticMethod = 0; +int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2. + +int methodOfDualTime = 3; +int min_sub_iter = 50; +int max_sub_iter = 50; +double tol_sub_iter = 0.01; + +int tscheme = 4; +int iSimplifyViscousTerm = 1; +int ifLocalTimeStep = 0; +int isUseLocalCFL = 0; +int isUsePreTwall = 0; +double CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; +double pMaxForCFL = 0.2; +double pMinForCFL = 0.1; +double deltaMaxForCFL = 0.2; +double magnifyFactorForCFL = 1.1; +double reduceFactorForCFL = 0.5; + +double ktmax = 1.0e10; + +int swapDq = 1; + +int nLUSGSSweeps = 1; +double LUSGSTolerance = 0.01; +int order = 2; + +double visl_min = 0.01; +double turbCFLScale = 1.0; +double csrv = 1.0; +double timemax = 1.0e10; +double dtsave = -1.0; +int maxale = 10; +double dtau = 0.001; + +int wallFunctionType = 0; + +int RKStage = 2; +double lamda[] = [0.5, 1.0]; + +//int RKStage = 1; +//double lamda[] = 1.0; + +//int RKStage = 4; +//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; +#************************************************************************ +# File In or Out * +#************************************************************************ +// numberOfGridGroups: The number of grid groups. +// gridfile: The partitioned Grid file path, using relative path, +// which is relative to the working directory. +// IMPORTANT WARNING: The file index should be ignored, +// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts, +// please use 'rae2822_hybrid2d__4.fts' here! +// plotFieldType: If dump out the field results to visulization. +// walldistMethod: The method to compute wall distance. +// 0 -- accurate but not fast enough. +// 1 -- fast but not accurate enough. +// 2 -- super fast but more non-accurate! +// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps. +// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps. +// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps. +// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps. +// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps. +// visualfile: The visualization file path of flowfield, write data for every default (intervalStepPlot) steps. +// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. +// nIsComputeWallDist: Whether to compute the wall distance. +// 0 -- Compute wall distance. +// 1 -- Not compute. +// protectionFile0 and protectionFile1: Two continuation file of the data protection mechanism. +// wall_heatfluxfile: The file to output the MaxHeatFlux of wall. +int numberOfGridGroups = 1; +string gridfile = "./grid/rae2822_hybrid2d__4.fts"; +string wallTemperaturefile = ""; + +int nIsComputeWallDist = 0; +int walldistMethod = 1; +int cellMethodOrNodeMethod = 0; + +string resSaveFile = "results/res.dat"; +string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; +string aircoeffile = "results/aircoef.dat"; + +string restartNSFile = "results/flow.dat"; +string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; + +string visualfile = "results/tecflow.plt"; +string wall_aircoefile = "results/wall_aircoef.dat"; +string samplefile = "results/sample.dat"; + +string protectionFile0 = "results/flow0.dat"; +string protectionFile1 = "results/flow1.dat"; +string wall_heatfluxfile = "results/wall_heatflux.dat"; + +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; + +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; + +string sixDofFileName = "results/sixDofInfo.dat"; +string derivativeFileName = "results/identify.dat"; +string hysteresisFileName = "results/force_beta.plt"; + +int plotFieldType = 0; + +// visualfileType: The file type of visualfile. +// 0 -- Tecplot binary. +// 1 -- Tecplot ASCII. +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. +int visualfileType = 1; + +// samplefileMode: The dump mode of sample file. +// 0 -- dump out every probe/line/surface data for all step intervals. +// 1 -- dump out all probe/line/surface data for every step intervals. +int samplefileMode = 0; + +// visualSlice: The slice of tecflow. +// 0 -- Do not save slice data. +// 1 -- comput and save it to sliceFile. +// sliceAxis: Normal vector of slice. +// 1 -- X_DIR. +// 2 -- Y_DIR. +// 3 -- Z_DIR. +// slicePostion: Coordinate of slice. + +int visualSlice = 0; +int sliceAxis = 1; +double slicePostion = -0.5; +string sliceFile = "results/Slice.plt"; +int dumpWallFaceCenter = 0; + +// min-max box of the visual block. +double lowerPlotFieldBox[] = [0.0 0.0 0.0]; +double upperPlotFieldBox[] = [1.0 1.0 1.0]; + +//-----------the optional parameters list for the flow field output---------------- +// nVisualVariables: Number of variables want to be dumped for tecplot visualization. +// visualVariables : Variable types dumped, listed as following: +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- viscosityLaminar(7), viscosityTurbulent(8), +// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12), +// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), +// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). +// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! +// Variables order must from small to big. +//-----------the optional parameters list for the wall boundary condition---------------- +// nVisualWallVariables: The number of visual variables on wall. +// visualWallVariables : dumped variable types, listed as following: +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- heat flux of species diffusion term(Qs, 9), heat flux of vibrational temperature term(Qv, 10), heat flux of electron temperature term(Qe, 11), +// -- species mass fractions(Ns, 12), x component of wall velocity(Vx, 13), y component of wall velocity(Vy, 14), z component of wall velocity(Vz, 15), +// -- slip translational-rotational temperature(Tts, 16), slip vibrational temperature(Tvs, 17), slip electron temperature(Tes, 18), absolute wall velocity(Vs, 19), +// -- Stanton number(St, 20), coefficient of heat rate(Ch, 21), temperature jump(deltaT, 22), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). +int nVisualVariables = 8; +int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; + +int nVisualWallVariables = 9; +int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; + +// dumpStandardModel: Dump many standard model data. +// 1 -- Turbulent flat plate. +int dumpStandardModel = 0; + +// ifSetDataMonitor: Whether to set the data monitor. +// 0 -- No. +// 1 -- Yes. +// dataMonitorType: The type of data Monitor. +// 0 -- Probes data monitor. +// 1 -- Lines data monitor. +// 2 -- Surfaces data monitor. +// probesDefineFile: Probes location information file. +// nLines: The number of lines need to be monitored. +// linesDefineFile: Lines location information file. +// nSurfaces: The number of surfaces need to be monitored. +// surfacesDefineFile: Surfaces location information file. +// searchCellsMethod: method to search the cell of each probe. +// 0 -- Nearest cell to the probe. +// 1 -- Real cell where the probe is located. +// nProbeVariables: Number of variables want to be dumped for probes monitered. +// probeVariables : Variable types dumped, listed as following: +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). +// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!! +// probeVariables order must from small to big. +// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables. +// 0 -- Take the value of probe's cell as probe real value. +// 1 -- Interpolation from probe's and neighbouring cell to probe. +// 2 -- Interpolation from probe's cell nodes to probe. +int ifSetDataMonitor = 0; + +int dataMonitorType = 0; +string probesDefineFile = "bin/probes_XYZ.dat"; + +//int dataMonitorType = 1; +//int nLines = 1; +//string linesDefineFile = "bin/lines_XYZ.dat"; + +//int dataMonitorType = 2; +//int nSurfaces = 4; +//string surfacesDefineFile = "bin/surfaces_XYZ.dat"; + +int searchCellsMethod = 0; + +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ +// turbInterval: Iteration number of turbulence. +// kindOfTurbSource: Kinds of turbulent source. +// 0 -- Original. +// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. +// transitionType: transition model type +// 0 -- none. +// 2 -- gama-re-theta. +// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition. +// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not. +int turbInterval = 1; +int turbOrderStruct = 2; +int kindOfTurbSource = 0; +int mod_turb_res = 0; +double freeStreamViscosity = 1.0e-3; +double muoo = 3.0; +double kwoo = 5.0; +int transitionType = 0; +double turbIntensity = -1.0; +int freeturbIntensitySRModify = 0; +double freeDecayXLocation = 0.0; +int compressibleCorrection = 0; +int transitionMaFix = 1; + +// maximum eddy viscosity (myt/my) max. +double eddyViscosityLimit = 1.0e10; +int monitor_vistmax = 0; + +#************************************************************************ +# LES Parameter * +#************************************************************************ +// iLES: Create LESSolver or not. +// = 1 -- Create LESSolver; +// != 1 -- not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 -- in only first sub-iter; +// != 0 -- in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 -- not; +// != 0 -- Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// sgsmodel: subgrid scale model. +// = "smagorinsky"; +// = "dsmCom"; +// = "wale"; +// = "sigma". +// deltaFunctionType: = 1 -- MAX(deltai, deltaj, deltak); +// = 2 -- pow(deltai * deltaj *deltak, 1/3); +// = 3 -- Devloped by Scotti. +// wallDampingFunctionType: = 0 -- no wall function; +// = 1 -- van Driest; +// = 2 -- developed by Dr. Deng Xiaobing; +// = 3 -- developed by Piomelli. +// turbViscousCutType: turbulent viscosity cut type. +// = 0 -- mu_total = mut + mul; +// = 1 -- mu_total = max(mut-mul, 0) + mul; +// = 2 -- mu_total = max(mut , 0) + mul. +// smagConstant: constant of smagorinsky model. +// waleConstant: constant of wale model. +// filterDirection [3]: filter variables in i, j, k direction or not. +// averageDirection[3]: average variables in i, j, k direction or not. +// isotropicConstant: constant of isotropic part of SGS stress. +int iLES = 0; +string sgsmodel = "smagorinsky"; +int deltaFunctionType = 2; +int wallDampingFunctionType = 1; +int turbViscousCutType = 2; +double smagConstant = 0.1; +double isotropicConstant = 0.0; +double waleConstant = 0.6; +double sigmaConstant = 1.35; +int filterDirection[] = [1, 1, 0]; +int averageDirection[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +#************************************************************************ +# Other Parameters for Hypersonic Non-equilibrium Gas * +#************************************************************************ +// dg_high_order: +// 0 -- generic order accuracy. +// 1 -- high order accuracy. +// iapplication: +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, +// nm: Equation number of the physics, but is out of commision now. +// 4 -- for 2D. +// 5 -- for 3D. +// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas. +// Otherwise, the pure gas with one component is used for perfect gas. +// 0 -- Earth gas. +// 1 -- Mars gas. +// 2 -- Argon. +// 3 -- Nitrogen. +// nEnergyRecycle: The type of EnergyModel Recycle. +// 0 -- not used. +// 1 -- used. +// nDensityModify: The type of densitymodify. +// 0 -- not used. +// 1 -- used. +// nchem: +// 0 -- without chemical reaction flow. +// 1 -- the chemical reaction flow is considered. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. +// 0 -- perfect gas. +// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nchemsrc: +// 0 -- the source terms are not computed. +// 1 -- the source terms are computed. +// nchemrad: +// 0 -- compute the spectrum radius without considering chemical reaction flow. +// 1 -- compute the spectrum radius that need to count the contribution from chemical reaction flow. +// ntmodel: The thermodynamic temperature model. +// 1 -- One-temperature model. +// 2 -- Two-temperature model. +// 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. +// nIdealState: whether take all gas species as ideal gas for gas-mixture process. +// 0 -- No. +// 1 -- Yes. // nTEnergyModel: the method to computing temperature energy model. +// 0 -- the energy term is computed using the conventional method. +// 1 -- the energy term is computed using the polynomial fitting method. +// 2 -- the energy term is computed using the piecewise polynomial fitting method. +// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model. +// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value. +// catalyticCoef: +// 0.0 -- full non-catalytic wall boundary condition. +// 1.0 -- full catalytic wall boundary condition. +// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// nTemperatureJump: the method to calculate the temperature jump. +// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode. +// 1 -- the general method where the iteration is calculated with the translation-rotation temperature. +// nSurfGradMethod: the method to compute the surface heating ratio. +// 0 -- the gradient of variable is computed with the first-order difference method. +// 1 -- the gradient of variable is computed with the Green-Guass integral method. +// nRapidFlowfield: initialize the flowfield using the rapid engineering method when it is greater than zero. +// nSurfHeatMonitor: To exam the surface heating change or not. 0 is no, 1 is yes. +// nInitPressureStep: the steps to initialize the boundary variables when the rapid method is used. 100 is the default value. +// nDumpCFLNumber: 1 indicates dumping the CFL number to file, 0 denotes no dumping. +// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0]. +// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0]. +// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0]. +// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// spectrumRadiusCoef: The value is in range of [0.0, 2.0]. +// staticPressureRelaxCorf: The value is in range of [0.1, 1.0]. +// nIsChemicalFreeze: the flag to freeze the chemical reactions. +// 0 -- not freeze, the chemical reaction sources will be calculated. +// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated. +// veTemperatureMin: The minimum of Tv and Te. +// maxViscous: the maximum of Viscous. +// trTemperatureMin: the minimum value of trTemperature. +// veTemperatureMin: the minimum value of veTemperature. +// densityMin: the minimum value of density. +// tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0]. +// nDebug: cout the Wrong place and abort +// 0 -- not used. +// 1 -- used. +// nSpeciesLimit: limitter of gas species +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid. +// 0 -- not used. +// 1 -- used. +// nViscosityPeModified: Pe Modified for ViscosityCoef. +// 0 -- not used. +// 1 -- used. +// nChemcalSourceModified: Modified on ChemcalSource. +// 0 -- not used. +// 1 -- used. +// nChemcalSourceEsMethod: Modified on ChemcalSource. +// 0 -- approximation algorithm 1 (Ori). +// 1 -- approximation algorithm 2 (New). +// nMaxStepTemperature: the iterative steps of temperature. +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. +// nAblation: +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. +// isInjection: +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. +// nViscosityModel: +// 0 -- Blottner fitting method(N89). +// 1 -- Gupta fitting method(N90). +// nContinueModel: The new continue model can switch different computation model. +// 0 -- Not use the new continue model. +// 1 -- use the new continue model. +// nSutherland: +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. +// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11". +// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. +// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. +// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "Gas-Mixture" -- indicates the process of mixing gas without reacting. +// for struct solver mixing two species��SpeciesA, SpeciesB��. +// for unstruct solver mixing multi-species��O2 NO CO CO2 H2 N2 Air CH4��. +// For self-definition model, the gasfile is used to indicate the file path of the new gas model. +// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. +// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. +// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes. +// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation. +// nIterSecondStep: the maximum number of iteration in the second step for the self-adaptive calculation. +// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation. +// nEnergyAssembly: the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory. +// 0 -- no, +// 1 -- yes. +// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model. +// 0 -- the density. +// 1 -- the translation temperature. +// 2 -- the vibration temperature. +// 3 -- the electron temperature. +// 4 -- the pressure. +// 5 -- the mass fraction of oxygen. +// 6 -- the mass fraction of nitrogen. +// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. +// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. +// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. +int dg_high_order = 0; +int iapplication = 0; +int isAdaptiveSolver = 0; +int nm = 5; +int nEquilibriumGas = 0; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; +int nIterFirstStep = 1000; +int nIterSecondStep= 2000; +int nIterThirdStep = 2000; +int nEnergyAssembly = 0; +int nControlVariable = 1; +double firstStepError = 0.01; +double secondStepError = 0.001; +double thirdStepError = 0.001; +double predictCFLError = 0.1; + +double refGama = 1.4; +double prl = 0.72; +double prt = 0.90; +double sc_l = 0.5; +double sc_t = 0.5; + +int nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; + +int nIdealState = 0; +int nEnergyRecycle = 1; +int nSlipBCModel = 0; +int nDensityModify = 1; +int nTEnergyModel = 0; +int nMeanFreePathType = 0; +int nIsChemicalFreeze = 0; +int nIsSuperCatalytic = 1; +int nTemperatureJump = 0; +int nSurfGradMethod = 0; +int nRapidFlowfield = 0; +int nSurfHeatMonitor = 0; +int nInitPressureStep = 100; +int nDumpCFLNumber = 0; + +double parkVDPower = 0.6; +double catalyticCoef = 0.0; +double sigmaVelocity = 1.0; +double sigmaTemperature = 1.0; +double sigmaMassFraction = 1.0; +double velocitySlipCorrectConstant = 1.0; + +double chemicalRelaxCorf = 1.0; +double chemicalSpectrumRadiusCoef = 1.0; +double viscousSpectrumRadiusCoef = 1.5; +double inviscidSpectrumRadiusCoef = 1.5; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; + +double maxViscous = 10000.0; +double trTemperatureMin = 10.0; +double veTemperatureMin = 30.0; +double maxTemperature = 50000.0; +double densityMin = 1.0e-8; +double densityMinFactor = 0.1; +double tAdjustmentFactor = 10.0; +double iniSpeedCoef = 1.0; +int iniSpeedMode = 0; + +int nDebug = 0; +int nSpeciesLimit = 1; +int nTurblenceForChemical = 0; +int nViscosityFluxSublevelModified = 1; +int nViscosityPeModified = 0; +int nChemcalSourceModified = 2; +int nChemcalSourceEsMethod = 1; +int nMaxStepTemperature = 5; +int veTemperatureMinModified = 1; +int nDiagonalModified = 0; +int nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; + +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +string speciesName = "O, O2, NO, N, N2"; +string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; + +//string speciesName = "O, O2, NO, N, NO+, N2, e-"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0"; + +//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0"; + +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + +//string gasfile = "Pa"; +//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0"; + +//string gasfile = "Combustion-12"; +//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; + +//string gasfile = "Gas-Mixture"; +//string speciesName = "SpeciesA, SpeciesB"; +//string initMassFraction = "1.0, 0.0"; +int nSutherland = 0; +double gamaSpeciesA = 1.4; +double gamaSpeciesB = 1.3; +double molecularWeightSpeciesA = 29.0; +double molecularWeightSpeciesB = 30.0; + +//string gasfile = "Gas-Mixture"; +//string speciesName = "O2, N2"; +//string initMassFraction = "1.0, 0.0"; + +int nFraction = 0; +int nContinueModel = 0; +int nChemicalFlowStep = 0; +int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; + +######################################################################### +// Multi-Grid parameters. +// nMGLevel: The number of level of Multi-Grid. +// <= 1 -- Single-level. +// > 1 -- multi-level. +// MGPreIteration: For each grid, the number of pre-smoothing steps. +// n_post: For each grid, the number of post-smoothing steps. +// MGCoarsestIteration: For the coarest grid the number of smoothing steps. +// MGFasType: V-multi cycle or W-multi cycle. +// 1 -- V-multi cycle. +// 2 -- W-multi cycle. +// flowInitStep: Flow initialization step, 0 - 500 is suggested. +// Multi-Grid : Number of steps computing on coarse grid, during flow initialization. +// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization. +// mgCFLScale: CFL number enlarge times for coarse grid. +// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid. +// 1 -- zero order. +// 2 -- first-order. (default) +// mgCorrectionLimit: Multi-grid correction limit. +int nMGLevel = 1; +int MGCoarsestIteration = 1; +int MGPreIteration = 1; +int MGFasType = 1; +int n_post = 0; +int flowInitStep = 100; +int mprol = 2; +double mgCFLScale = 1.0; +double mgCorrectionLimit = 0.01; + +//--------------- Some parameter for turbulent model -------------------- +// neasm: The variation of kw turbulent model. +// ismooth_turb: Residual smooth for turb or not. +// SSTProductType: The type of product term based on vorticity for SST. +// SAProductType: The type of product term based on vorticity for SA. +int neasm = -3; +int SSTProductType = 0; +int ismooth_turb = 0; +int SAProductType = 2; + +// ----------------- Overset Grid parameter ----------------------------- +int codeOfDigHoles = 1; +int codeOfTurbulentModel = 0; +string masterFileName = "./grid/searchFile.inp"; +string holeBasicFileName = "./grid/holeBasicFile.inp"; +string holeFullFileName = "./grid/holeFullFile.dat"; +string linkFileName = "./grid/topology.dat"; +string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; + +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ +// isFVMOrFDM: +// 0 -- NSSolverStruct using Finite Volume Method. +// 1 -- NSSolverStruct using Finite Differ Method. +// SolverStructOrder: Spatial discretisation order of NS equations with struct grid. +// <= 2 -- finite volume method. +// >= 3 -- finite difference order. (to be completed) +// 0 -- default. +// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence, +// smaller epsilon, robuster for shock-detecting. +// str_highorder_interpolation_type: +// -- "classical", "test". +// str_highorder_flux_name: +// -- "roe", "steger". +// structhighordergradient: +// -- "conservation", "chain_rule". +int isFVMOrFDM = 0; +string str_highorder_solver = "WCNS"; +int SolverStructOrder = 0; +double str_highorder_interpolation_epsilon = 1.0e-6; +string str_highorder_interpolation_type = "test"; +string str_highorder_flux_name = "steger"; +string structhighordergradient = "conservation"; +double coefofstrflux = 0.5; +double limitcoefofinterface = 0.0; + +// ----------------- Advanced choices ----------------------------------- +// outtimesc: Time stepping scheme for the outer loop. +// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1]. +// -1 -- seconde-order fully-upwind differencing. +// 0 -- seconde-order upwind-biased differencing. +// 0.333333 -- third-order upwind-biased differencing. +// 1 -- seconde-order central differencing. +// MUSCLCoefXb: The limiter parameter. +// 0 -- the effect of the limiter is cancelled, means the first-order interpolations. +// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1. +string outtimesc = "impbd2"; +double MUSCLCoefXk = -1; +double MUSCLCoefXb = 1.0; +int allReduceStep = 1; + +// ----------------- overlap configuration ------------------------------ +// codeOfOversetGrid: Overlapping(overset) grid or not. +// 0 -- NON-overlapping grid. +// 1 -- Overlapping grid. +// oversetInterpolationMethod: the method of overset interpolation while field simulation. +// 0 -- set the acceptor cell value by donor cell value. +// 1 -- set the acceptor cell value by distance weight of donor cell value. +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.ovs"; +double walldistMainZone = 1.0 +double toleranceForOversetSearch = 1.0e-3; +double toleranceForOversetBox = 1.0e-3; +int twoOrderInterpolationOrNot = 0; +int keyEnlargeOfActiveNodes = 0; +int outTecplotOverset = 0; +int outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; + +// ----------------- ALE configuration ------------------------------ +int codeOfAleModel = 0; +int aleStartStrategy = -1; + +double referenceLength = 1.0; +double referenceVelocity = 1.0; +double referenceDensity = 1.0; + +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. + +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. +int methodForKineticEquation = 0; +double relaxParameterOfKinetic = 1.0; + +#************************************************************************ +# motive information * +#************************************************************************ +int numberOfMovingBodies = 1; + +############################## body0 ############################## +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. +// -1 given motion partten. +// 0 still. +// 1 six DOF motion. +// 2 three DOF motion. +// 11 X-axis forced motion. +// 12 Y-axis forced motion. +// 13 Z-axis forced motion. +// 14 forced pitch motion. +// 15 forced yaw motion. +// 16 forced roll motion. +int RBDMethod_0 = 0; +double amplitude_0 = 0.0; +double reduceFrequency_0 = 0.0; +// direction of rotation. +// 1 -- clockwise from the point of view along the positive x axis. +// -1 -- anticlockwise from the point of view along the positive x axis. +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; + +// post indentify. +int integralOrder = 4; + +// ---------------- ATP read -------------------------------------------- +//@int inflowParaType = 0; +//@double refReNumber = 6.5e6; +//@double refDimensionalTemperature = 288.15; +//@double freestream_vibration_temperature = 300.00; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalVelocity = 0; +//@double refDimensionalDensity = 0; +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ +int isPlotVolumeField = 0; + +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; + +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; + +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ +int isSolveEnergyEquation = 0; +int isSolveTurbEquation = 0; +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/L05_TwoD_Cavity_BGK_OMP_1CPU/bin/input.txt b/L05_TwoD_Cavity_BGK_OMP_1CPU/bin/input.txt new file mode 100644 index 0000000..f567ed4 --- /dev/null +++ b/L05_TwoD_Cavity_BGK_OMP_1CPU/bin/input.txt @@ -0,0 +1,33 @@ +0 ！MRT set 1, BGK set 0 +1 ic.plt ！CONTI, resume :1 , new 0 //follows input datafile name +0 ！LES yes: 1 , no: 0 +0 mesh_3d.dat ！GEO read complex geo? yes:1, no:0 //follows input datafile name +0 ! MB multiblock LBM? yes:1, no:0 +0 2.e-3 !CONV using converge criterion? yes:1, no:0 +201 ！NX +201 ! NY +1 ! NZ +240 ！ NX2 +160 ！ NY2 +1 ! NZ2 +500 ! LowX +160 ! LowY +0 ! LowZ +200 ! framerate +50000 ！total steps to terminate +1.0 ! density +0.8 ！ tau +(0.0, 0.0, 0.0000000) ！ Volumetric force vector (gx, gy, gz) +D2Q9 ! velocity set +Cavity ! boundary condition +! note: in the following, boundary types: periodic,velocity, pressure +! are allowed. if "velocity" is applied, please strictly follow the format "velocity (%lf, %lf, %lf)". +nonslip ！xmin face +nonslip ！xmax face +nonslip ！ymin face +velocity (0.1, 0.00, 0.0) ！ymax face, +nonslip ！zmin face +nonslip ！zmax face +-------------------！ initial velocity field +(0.0, 0.00, 0.0) + diff --git a/L05_TwoD_Cavity_BGK_OMP_1CPU/bin/key.hypara b/L05_TwoD_Cavity_BGK_OMP_1CPU/bin/key.hypara new file mode 100644 index 0000000..9470ea6 --- /dev/null +++ b/L05_TwoD_Cavity_BGK_OMP_1CPU/bin/key.hypara @@ -0,0 +1,58 @@ +string title = "PHengLEI Main Parameter Control File"; + +// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE. +string defaultParaFile = "./bin/cfd_para.hypara"; + +// ndim: Dimensional of the grid, 2 or 3. +// nparafile: the number of parameter files. +// nsimutask: simulation task type. +// 0 -- CFD Solver of NS or Turbulation. +// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc. +// Grid conversion: from other format to PHengLEI format (.fts). +// Grid reconstruction: such as grid adaptation. +// Grid merging: merge two blocks into one block. +// Grid repairing: repair the original grid in order to remove the negative volume cells. +// 2 -- Wall distance computation for turb-solver. +// 3 -- Grid partition. +int ndim = 2; +int nparafile = 1; + +//int nsimutask = 0; +//string parafilename = "./bin/cfd_para_subsonic.hypara"; +//string parafilename = "./bin/cfd_para_transonic.hypara"; +//string parafilename = "./bin/cfd_para_supersonic.hypara"; +//string parafilename = "./bin/cfd_para_hypersonic.hypara"; +//string parafilename = "./bin/cfd_para_incompressible.hypara"; + +//int nsimutask = 1; +//string parafilename = "./bin/grid_para.hypara"; + +//int nsimutask = 2; +//string parafilename = "./bin/cfd_para.hypara"; + +//int nsimutask = 3; +//string parafilename = "./bin/partition.hypara"; + +//int nsimutask = 1; +//string parafilename = "./bin/grid_deform_para.hypara"; + +//int nsimutask = 1; +//string parafilename = "./bin/grid_refine_para.hypara"; + +//int nsimutask = 5; +//string parafilename = "./bin/overset_grid_view.hypara"; + +int nsimutask = 17; +string parafilename = "./bin/cfd_para.hypara"; + +//int nsimutask = 14; +//string parafilename = "./bin/integrative_solver.hypara"; + +//int nsimutask = 99; +//string parafilename = "./bin/post_processing.hypara"; + +// ---------------- Advanced Parameters, DO NOT care it ---------------- +int numberOfGridProcessor = 0; +// ATP read +//@string parafilename1 = "" +//@string parafilename2 = ""; diff --git a/L06_TwoD_Spoiler_BGK_OMP_4CPU/bin/cfd_para.hypara b/L06_TwoD_Spoiler_BGK_OMP_4CPU/bin/cfd_para.hypara new file mode 100644 index 0000000..f903a5a --- /dev/null +++ b/L06_TwoD_Spoiler_BGK_OMP_4CPU/bin/cfd_para.hypara @@ -0,0 +1,1467 @@ +//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ +// PPPPP H H EEEEE N N GGGGG L EEEEE III + +// P P H H E NN N G L E I + +// PPPPP HHHHH EEEEE N N N G GG L EEEEE I + +// P H H E N N N G G L E I + +// P H H EEEEE N N GGGGG LLLLL EEEEE III + +//------------------------------------------------------------------------+ +// Platform for Hybrid Engineering Simulation of Flows + +// China Aerodynamics Research and Development Center + +// (C) Copyright, Since 2010 + +// PHengLEI 2212 + +//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ +########################################################################### +# Default parameters for Grid conversion # +########################################################################### +// gridtype: Grid type for generation, conversion, reconstruction, merging. +// 0 -- Unstructured grid. +// 1 -- Structured grid. +// 2 -- Hybrid grid, include both of unstructured and structured grid. +// gridobj: Task type of grid treatment. +// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc. +// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS. +// 2 -- Grid refinement. +// 3 -- Grid merging, merge two blocks into one block. +// 4 -- Grid deformation, achieve unstructured grid deformation. +// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells. +// 6 -- Grid mirroring, mirror a symmetry grid to whole grid. +// 7 -- Grid type change, convert structured grid to unstructured grid. +// multiblock: Multi-block grid or not, only for structured grid conversion. +// 0 -- Not. +// 1 -- Yes. +// iadapt: Adaptation number for unstructure grid. +// SymmetryFaceVector: The vector of symmetry face. +// 0 -- X axis. +// 1 -- Y axis. +// 2 -- Z axis. +// gridReorder: Reorder cell and face of grid or not, only for 3D unstructured grid conversion, +// which is CGNS type. +// 0 -- Not. +// 1 -- Yes. +// faceReorderMethod: the reorder method face of unstructured grid. +// 0 -- BSFCELLFACEORG. +// 1 -- BSFCELLFACELEFT. +// 2 -- BSFCELLFACERIGHT. +int gridtype = 0; +int gridobj = 1; +int multiblock = 0; +int iadapt = 0; +int SymmetryFaceVector = 1; +int gridReorder = 0; +int faceReorderMethod = 0; + +// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating. +// axisRotateOrder : axis rotating order. +// 1 -- X-axis. +// 2 -- Y-axis. +// 3 -- Z-axis. +// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order. +int nAxisRotateTimes = 0; +int axisRotateOrder[] = [1, 2, 3]; +double axisRotateAngles[] = [0.0, 0.0, 0.0]; + +// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". +// 0 -- Interface. (default) +// 1 -- Physical boundary condition, used in Hybrid solver. +int omit_no_bound_bc = 0; +int omitRepeatInterface = 1; + +//----------------------------------------------------------------------- +# Grid data type # +//----------------------------------------------------------------------- +// from_gtype/to_gtype: Type of grid data type in grid conversion process. +// -1 -- MULTI_TYPE. +// 1 -- PHengLEI, *.fts. +// 2 -- CGNS, *.cgns. +// 3 -- Plot3D type of structured grid, *.dat/*.grd. +// 4 -- Fieldview type of unstructured grid, *.dat/*.inp. +// 5 -- Fluent, *.cas/*.msh. +// 6 -- Ustar, mgrid.in. +// 7 -- Hybrid, include both of unstructured and structured grid, *.fts. +// 8 -- GMSH, *.msh. +// 9 -- Gridgen type of structured grid, *.dat/*.grd. +// dumpOldGrid: If dump out the old grid file. +// 0 -- Not. (default) +// 1 -- Yes. +int from_gtype = 2; +int to_gtype = 1; +int dumpOldGrid = 0; + +//----------------------------------------------------------------------- +# File path # +//----------------------------------------------------------------------- +// from_gfile: path of original data file for unstructure grid convert from. +// out_gfile: path of target file for grid convert to, *.fts type of file usually. +int numberOfGridFile = 1; +string from_gfile = "./grid/rae2822_hybrid2d.cas"; +string from_gfile1 = ""; +string out_gfile = "./grid/flat_laminr_133_85_2d.fts"; + +// ----------------- some advanced choices ------------------------------ +// iunsteady: The Grid is for unsteady simulation or not. +int iunsteady = 0; + +// fileformat: Ustar Grid file format. +// 0 -- BINARY. +// 1 -- ASCII. +int fileformat = 0; + +// Parameters for hybrid solver. +// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type. +// mixgrid_str: path of structure grid file for hybrid solver, *.fts type. +string mixgrid_uns = "./grid/rae2822_uns2d_4.fts"; +string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts"; + +// Some parameters for structured overlapping grid. +int codeOfDigHoles = 1; +string holeBasicFileName = "./oversetGridView/holeBasicFile.inp"; +string holeFullFileName = "./oversetGridView/holeFullFile.dat"; +string linkFileName = "./oversetGridView/topology.dat"; +string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp"; + +// ----------------- Grid Refine Parameters ----------------------------- +// anisoRefine: If refine grid by anisoRefine type. +// 0 -- Not. (default) +// 1 -- Yes. +// geometryUnit: Geometry unit. +// 1 -- meter. +// 2 -- millimeter. +// 3 -- inch. +// exclusiveCase: Parallel projection exclusive case. +// 0 -- NON case. +// 1 -- JSM-C2-NPOFF case. +// 2 -- CHNT. +// projectOrgPoint: If the original wall points need to be projected or not. +int anisoRefine = 0; +int geometryUnit = 1; +int isProject = 0; +int readDist = 0; +int isDeform = 0; +int exclusiveCase = 0; +int projectOrgPoint = 0; +string geometryFileName = "./grid/jsm.igs"; + +// ----------------- Grid Deform Parameters ----------------------------- +// deformationMethod: Grid Deform. +// 1 -- SPRING. +// 2 -- RBF. +// stationalGridFile: Original grid file. +// visualFileName : The visualization file path of deform grid. +// nDeformStep : The max deform step. +// flapAngle : The max flap angle. +// rotatePostionZ : Rotate postion. +// rotatePostionY : Rotate postion. +// gridSlice : If dump slice grid. +// sliceAxis : Grid slice axis. +// slicePosition : Grid slice position. +int nDeformStep = 40; +double flapAngle = 10.0; +double rotatePostionZ = 4.00003; +double rotatePostionY = 3.05; + +int deformationMethod = 2; +string stationalGridFile = "./grid/Segment2Brid.fts"; +string visualFileName = "./results/deformedGrid.dat" + +int gridSlice = 1; +int sliceAxis = 1; +double slicePosition = 13; + +// ----------------- RBF Parameters ------------------------------------- +// numberOfReferenceCP: Number of reference Control Points. +// influencePara : The RBF influence radius parameter. +int numberOfReferenceCP = 40; +double influencePara = 25.0; + +// ----------------- Periodic Parameters -------------------------------- +// Notice: Rotational periodicity only support rotation along the X axis! +// periodicType: Which periodic boundary is used. +// 0 -- without Periodic Boundary. +// 1 -- Translational periodicity. +// 2 -- Rotational periodicity. +// translationLength[]: The relative distance between two periodic face + which only support one direction. +// rotationAngle: The relative angle between two periodic face. + which is recorded in degrees. +int periodicType = 0; +double translationLength[] = [0.0, 0.0, 0.0]; +double rotationAngle = 0.0; + +######################################################################### +# Default parameters for Partition # +######################################################################### +// pgridtype: The grid type. +// 0 -- unstruct grid. +// 1 -- struct grid. +// 2 -- refine structured grid. +// maxproc: The number of partition zones that want to be divided into. +// numberOfMultifile: The number of partition grid files that want to be dumped out. +int pgridtype = 0; +int maxproc = 4; +int numberOfMultifile = 1; + +// traceMark: Trace mark or not, only for structured grid partition. +// 0 -- Not. +// 1 -- Yes. +// blockIndexOfMark: the block index of mark, only for structured grid partition. +// cellIndexOfMark : the cell index of mark, only for structured grid partition. +int traceMark = 0; +int blockIndexOfMark = 0; +int cellIndexOfMark[] = [185, 30, 1]; + +// parallelStrategy: +// 0 -- each zone is assigned to the one that defined in grid partition procedure. +// 1 -- random assigned for each zone or by some else ways. +int parallelStrategy = 1; + +//----------------------------------------------------------------------- +# File path # +//----------------------------------------------------------------------- +// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts). +// partition_grid_file: Target partition grid file(PHengLEI type, *.fts). +string original_grid_file = "./grid/sphere_mixed.fts"; +string partition_grid_file = "./grid/sphere_mixed__4.fts"; + +// ------------------ Sompe advanced parameters ------------------------- +// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition". +// 0 -- Interface. (default) +// 1 -- Physical boundary condition, used in Hybrid solver. +// npartmethod: Method of interface reconstruction, default is 1. +// parallelPartitionMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition. +// 1 -- Using ParMetis for homogeneous MPI. +// 2 -- Using Metis for homogeneous MPI. +// 3 -- using METIS partition for homogeneous OpenMP. +// parmetisBalance: Used to specify the imbalance tolerance. +// 1 -- perfect balance. +// maxproc -- perfect imbalance. +// 1.05 -- recommended. +int omit_no_bound_bc = 0; +int npartmethod = 1; +int parallelPartitionMethod = 2; +double parmetisBalance = 1.05; + +// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid. +// 1 -- single level. +// 2 -- 2 level. +// N -- N level, ..., et al. +int numberOfMultigrid = 1; + +######################################################################### +# Default parameters for CFD simulation # +######################################################################### +// maxSimuStep: The max simulation step, don't care simulation is restart or not. +// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved. +// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved. +// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved. +// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. +// intervalStepRes: The step intervals for residual file 'res.dat' saved. +int maxSimuStep = 20000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; +int intervalStepSample = 1000; +int intervalStepForce = 100; +int intervalStepRes = 10; + +// compressible: +// 0 -- incompressible flow. +// 1 -- compressible flow. (default) +int compressible = 1; + +// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow. +// 0 -- no precondition process. (default, mach > 0.3) +// 1 -- carry out precondition process. (mach number <= 0.3) +// Kprec: The coefficient K for the cut-off velocity. +// 1.0~3.0 is suggested. (default, 3.0) +// preconFarfieldBCMethod: The precondition method for farfield boundary condition. +// 0 -- precondition far-field boundary based on riemann invariants. +// 1 -- Turkel's simplified far-field boundary condition. +int ifLowSpeedPrecon = 0; +double Kprec = 3.0; +int preconFarfieldBCMethod = 1; + +//----------------------------------------------------------------------- +# CFD Control Parameter # +//----------------------------------------------------------------------- +// refMachNumber: Mach number. +// attackd: Angle of attack. +// angleSlide: Angle of sideslip. +// inflowParaType: The type of inflow parameters. +// 0 -- the nondimensional conditions. +// 1 -- the flight conditions. +// 2 -- the experiment conditions. +// 3 -- the subsonic boundary conditions. (Useless!) +// 4 -- the condition that the velocity, temperature and density are given. +// 5 -- the condition that the velocity, temperature and pressure are given. +//flowInitMethod: Flow field initialization method. +// 0 -- The entire flow field is initialized according to Infinite velocity. +// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate. +// refReNumber: Reynolds number, which is based unit length, unit of 1/m. +// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition. +// freestream_vibration_temperature: Dimensional freestream vibration temperature. +// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition. +// height: Fly height, unit of km. +// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition. +// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter. Common dimensions like: +// 1 dm = 0.1 m. +// 1 cm = 0.01 m. +// 1 mm = 0.001 m. +// 1 inch = 0.0254 m. +// 1 foot = 12 inches = 0.3048 m. +// 1 yard = 3 feet = 0.9144 m. +// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit. +// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit. +// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary +// condition is radiation equilibrium temperature, and 0.8 is the default value. +// refMolecularWeight: the reference molecular weight of gas used for perfect gas. The unit is g/mol. +// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on. +int directionMethod = 0; +double refMachNumber = 0.73; +double attackd = 2.79; +double angleSlide = 0.00; +int flowInitMethod = 0; + +int inflowParaType = 0; +double refReNumber = 6.5e6; +double refDimensionalTemperature = 288.15; +double freestream_vibration_temperature = 300.00; + +//int inflowParaType = 1; +//double height = 0.001; + +//int inflowParaType = 2; +//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2). +//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)). + +// The velocity, temperature and density are fixed. +//int inflowParaType = 4; +//double refDimensionalVelocity = 1000.0; +//double refDimensionalDensity = 1.0e3; + +// The velocity, temperature and pressure are fixed. +//int inflowParaType = 5; +//double refDimensionalVelocity = 1000.0; +//double refDimensionalPressure = 1.0e5; + +// The MachNumber, temperature and pressure are fixed. +//int inflowParaType = 6; +//double refDimensionalTemperature = 293.0; +//double refDimensionalPressure = 8886.06; + +// The velocity, temperature and pressure are read from file. +//int inflowParaType = 7; +//string weatherDataFilePath = "./WRFData/"; +//double longitude = 110.95 +//double latitude = 19.61; + +double wallTemperature = -1.0; + +double radiationCoef = 0.8; +double gridScaleFactor = 1.0; +double gridTranslationVector[] = [0.0, 0.0, 0.0]; + +int numberOfAerodynamicForceComponents = 1; +double forceReferenceLengthSpanWise = 1.0; // unit of meter. +double forceReferenceLength = 1.0; // unit of meter. +double forceReferenceArea = 1.0; // unit of meter^2. +double TorqueRefX = 0.0; // unit of meter. +double TorqueRefY = 0.0; // unit of meter. +double TorqueRefZ = 0.0; // unit of meter. +double knudsenLength = 1.0; // unit of meter. +double refMolecularWeight = 28.9644; // unit of g/mol. + +//----------------------------------------------------------------------- +# Spatial Discretisation # +//----------------------------------------------------------------------- +#************************************************************************ +# Struct Solver * +#************************************************************************ +// inviscidSchemeName: Spatial discretisation scheme of struct grid. +// Using this when solve structered grid or hybrid. +// -- "vanleer", "steger", "hlle", "lax_f", +// -- "roe", "modified_roe", +// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+". +// isWennScheme: If using WENN Scheme of struct grid. +// 0 -- NO. (default) +// 1 -- Yes. +// str_limiter_name: Limiter of struct grid. +// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth", +// -- "nolim", no limiter, +// -- "vanalbada_clz", clz supersonic version, +// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3". +string inviscidSchemeName = "roe"; +int isWennScheme = 0; +string str_limiter_name = "vanalbada"; + +#************************************************************************ +# UnStruct Solver or Common * +#************************************************************************ +// viscousType: Viscous model. +// 0 -- Euler. +// 1 -- Lamilar. +// 2 -- Algebraic. +// 3 -- 1eq turbulent. +// 4 -- 2eq turbulent. +// viscousName: Laminar or tubulent model. +// -- "0eq-bl". +// -- "1eq-sa". +// -- "2eq-kw-menter-sst". +// -- "2eq-kw-menter-bsl". +// -- "2eq-kw-wilcox-1988". +// -- "2eq-kw-wilcox-1998". +// -- "2eq-kw-kok-tnt". +// -- "2eq-kw-wilcox-2006". +// -- "easm-kw-2003". +// -- "easm-kw-2005". +// DESType: Type of DES. +// 0 -- RANS. (default) +// 1 -- DES. +// 2 -- DDES. +// 3 -- IDDES. +// uns_scheme_name: Spatial discretisation scheme of Unstruct grid. +// Using this when solve Unstructered grid or hybrid. +// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle", +// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+". +// uns_limiter_name: Limiter of Unstruct grid. +// -- "barth", "vencat", "vanleer", "minmod", +// -- "vanalbada", "smooth", "nnd", "lpz", "1st", +// -- "nolim", no limiter. +// uns_vis_name: Discretisation method of viscous term. +// -- "std", "test", "aver", "new1", "new2". +// gradientName: Gradient reconstruction method. +// -- "default", "ggcell", "ggnode", "lsq". +// ivencat: Variation of vencat limiter. +// 0 -- org method, it is independent of grid scale. +// 1 -- new method, it is dependent of grid scale. +// 4 -- Ustar limiter model, without grid size unitary. +// 7 -- default used. +// venkatCoeff: Cofficient of vencat, when using vencat limter. +// limitVariables: Limit model (It is useful only if limitVector is 0). +// 0 -- limit only for pressure and denstiny, then get the min value. +// 1 -- limit for every variables, then get the min value. +// limitVector: +// 0 -- Each variable use the same limiter coefficient. +// 1 -- Each variable use the respective limiter coefficients. +// reconmeth: +// 0 -- When reconstruct face value, Q+, Q- use respective limiter coefficients. +// 1 -- Q+, Q- use the min limiter coefficients of left and right cell. +// skewnessAngle: The skewness angle of grid cells. +// roeEntropyFixMethod: Entropy fix (correction) method. +// 1 -- direct fix, which limits the minimum eigenvalue directly. +// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver. +// 3 -- Harten type, which is default used. +// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0. +// It is used to scale the default Roe entropy fix coefficients. +// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0. + +//int viscousType = 0; +//string viscousName = "Euler"; + +//int viscousType = 1; +//string viscousName = "laminar"; + +int viscousType = 3; +string viscousName = "1eq-sa"; + +//int viscousType = 4; +//string viscousName = "2eq-kw-menter-sst"; + +int DESType = 0; + +string uns_scheme_name = "roe"; +string uns_limiter_name = "vencat"; +string uns_vis_name = "test"; +string gradientName = "ggnode"; + +int ivencat = 7; +double venkatCoeff = 5.0; +int reconmeth = 1; +int limitVariables = 0; +int limitVector = 0; +double skewnessAngle = 60.0; + +int roeEntropyFixMethod = 3; +double roeEntropyScale = 1.0; + +double AusmpwPlusLimiter = 1.0; + +#************************************************************************ +# Temporal Discretisation * +#************************************************************************ +// iunsteady: Steady or unsteady. +// 0 -- steady. +// 1 -- unsteay. +// physicalTimeStep: The nondimensional physical time step. +// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes. +// ifStaticsFlowField: Statistical variables for unsteady simulation. +// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation. +// startStatisticStep: Outer step when start statistics. +// when the value is larger than "maxSimuStep", it is useless. +// statisticalTimePeriod: Used as time period of statistic analysis. +// when the value is negative, time period is treated as infinite. +// statisticMethod: Statistic reynolds stress method. +// 0 -- tau = - ^2 +// 1 -- tau = +// min_sub_iter: The min sub iteration of unsteady simulation. +// max_sub_iter: The max sub iteration of unsteady simulation. +// tol_sub_iter: The tolerance of sub iteration of unsteady simulation. +// tscheme: Temporal Discretisation method. +// 1 -- Runge-Kutta Multi-State. +// 2 -- Point implicit. +// 3 -- Full implicit. +// 4 -- LU-SGS. +// 5 -- Block LU-SGS. +// 6 -- Jacobian iteration. +// 7 -- Line LU-SGS. +// 8 -- Matrix LU-SGS. +// 9 -- GMRES. +// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation. +// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method. +// CFLStart: Started cfl number. +// CFLEnd: End cfl number. +// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd. +// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration. +// OriginalTscheme : Used for LUSGS and GMres hybrid computing. +// useLUSGSprecond: Initialize flow field for GMRES. +// 0 --Initialize by first order Jacobian matrix. +// 1 --Initialize by LUSGS. +// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field. +// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i]) +// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0. +// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS. +// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS. +// ifLocalTimeStep: Time step method. +// 0 --Local. +// 1 --Global. +// isUseLocalCFL: use variable number of CFL or not. +// 0 -- global unified CFL number. +// 1 -- local CFL number. +// isUsePreTwall: use the previous temperatures on wall. 1 indicates yes, and 0 indicates no. +// visl_min: Minimum value of laminar viscosity coefficient. +// turbCFLScale: Turbulence model cfl number factor. +// codeOfAleModel: Arbitrary Lagrangian-Eulerian method. +// 0 -- no ALE method. +// 1 -- ALE method for non-moving grids. +// 2 -- ALE method for moving grids. +// 3 -- ALE method for deforming grids. +// wallFunctionType: The type of wall function to implement. +// 0 -- no wall function. (default) +// 1 -- standard wall function. +// 2 -- Pab3D wall function. +// RKStage: The number of Runge-Kutta step. +// lamda: Cofficient of Runge-Kutta step. +int iunsteady = 0; +double physicalTimeStep = 0.01; +double physicalTimeStepDimensional = -0.001; +int ifStartFromSteadyResults = 0; +int ifStaticsFlowField = 0; +int ifStaticsReynoldsStress = 0; +int startStatisticStep = 800000; +double statisticalTimePeriod = -1.0; +int statisticMethod = 0; +int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2. + +int methodOfDualTime = 3; +int min_sub_iter = 50; +int max_sub_iter = 50; +double tol_sub_iter = 0.01; + +int tscheme = 4; +int iSimplifyViscousTerm = 1; +int ifLocalTimeStep = 0; +int isUseLocalCFL = 0; +int isUsePreTwall = 0; +double CFLStart = 0.01; +double CFLEnd = 10.0; +int CFLVaryStep = 500; +double GMRESCFLScale = 1.0; +int OriginalTscheme = 9; +int useLUSGSprecond = 1; +int GMRESInitStep = 1000; +double pMaxForCFL = 0.2; +double pMinForCFL = 0.1; +double deltaMaxForCFL = 0.2; +double magnifyFactorForCFL = 1.1; +double reduceFactorForCFL = 0.5; + +double ktmax = 1.0e10; + +int swapDq = 1; + +int nLUSGSSweeps = 1; +double LUSGSTolerance = 0.01; +int order = 2; + +double visl_min = 0.01; +double turbCFLScale = 1.0; +double csrv = 1.0; +double timemax = 1.0e10; +double dtsave = -1.0; +int maxale = 10; +double dtau = 0.001; + +int wallFunctionType = 0; + +int RKStage = 2; +double lamda[] = [0.5, 1.0]; + +//int RKStage = 1; +//double lamda[] = 1.0; + +//int RKStage = 4; +//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0]; +#************************************************************************ +# File In or Out * +#************************************************************************ +// numberOfGridGroups: The number of grid groups. +// gridfile: The partitioned Grid file path, using relative path, +// which is relative to the working directory. +// IMPORTANT WARNING: The file index should be ignored, +// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts, +// please use 'rae2822_hybrid2d__4.fts' here! +// plotFieldType: If dump out the field results to visulization. +// walldistMethod: The method to compute wall distance. +// 0 -- accurate but not fast enough. +// 1 -- fast but not accurate enough. +// 2 -- super fast but more non-accurate! +// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps. +// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps. +// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps. +// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps. +// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps. +// visualfile: The visualization file path of flowfield, write data for every default (intervalStepPlot) steps. +// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. +// nIsComputeWallDist: Whether to compute the wall distance. +// 0 -- Compute wall distance. +// 1 -- Not compute. +// protectionFile0 and protectionFile1: Two continuation file of the data protection mechanism. +// wall_heatfluxfile: The file to output the MaxHeatFlux of wall. +int numberOfGridGroups = 1; +string gridfile = "./grid/rae2822_hybrid2d__4.fts"; +string wallTemperaturefile = ""; + +int nIsComputeWallDist = 0; +int walldistMethod = 1; +int cellMethodOrNodeMethod = 0; + +string resSaveFile = "results/res.dat"; +string turbresfile = "results/turbres.dat"; +string transitionResFile = "results/transitionRes.dat"; +string aircoeffile = "results/aircoef.dat"; + +string restartNSFile = "results/flow.dat"; +string turbfile = "results/turb.dat"; +string transitionFile = "results/transition.dat"; + +string visualfile = "results/tecflow.plt"; +string wall_aircoefile = "results/wall_aircoef.dat"; +string samplefile = "results/sample.dat"; + +string protectionFile0 = "results/flow0.dat"; +string protectionFile1 = "results/flow1.dat"; +string wall_heatfluxfile = "results/wall_heatflux.dat"; + +string protectionTurbFile0 = "results/turb0.dat"; +string protectionTurbFile1 = "results/turb1.dat"; + +string protectionTransitionFile0 = "results/transition0.dat"; +string protectionTransitionFile1 = "results/transition1.dat"; + +int nDumpSurfaceInfo = 0; +string wall_varfile = ""; + +string sixDofFileName = "results/sixDofInfo.dat"; +string derivativeFileName = "results/identify.dat"; +string hysteresisFileName = "results/force_beta.plt"; + +int plotFieldType = 0; + +// visualfileType: The file type of visualfile. +// 0 -- Tecplot binary. +// 1 -- Tecplot ASCII. +// 2 -- Ensight binary. +// 3 -- Ensight ASCII. +int visualfileType = 1; + +// samplefileMode: The dump mode of sample file. +// 0 -- dump out every probe/line/surface data for all step intervals. +// 1 -- dump out all probe/line/surface data for every step intervals. +int samplefileMode = 0; + +// visualSlice: The slice of tecflow. +// 0 -- Do not save slice data. +// 1 -- comput and save it to sliceFile. +// sliceAxis: Normal vector of slice. +// 1 -- X_DIR. +// 2 -- Y_DIR. +// 3 -- Z_DIR. +// slicePostion: Coordinate of slice. + +int visualSlice = 0; +int sliceAxis = 1; +double slicePostion = -0.5; +string sliceFile = "results/Slice.plt"; +int dumpWallFaceCenter = 0; + +// min-max box of the visual block. +double lowerPlotFieldBox[] = [0.0 0.0 0.0]; +double upperPlotFieldBox[] = [1.0 1.0 1.0]; + +//-----------the optional parameters list for the flow field output---------------- +// nVisualVariables: Number of variables want to be dumped for tecplot visualization. +// visualVariables : Variable types dumped, listed as following: +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- viscosityLaminar(7), viscosityTurbulent(8), +// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12), +// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), +// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), streamline_u(45), streamline_v(46), streamline_w(47), +// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52), +// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58), +// -- overlap iblank(iblank, 81), +// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62). +// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!! +// Variables order must from small to big. +//-----------the optional parameters list for the wall boundary condition---------------- +// nVisualWallVariables: The number of visual variables on wall. +// visualWallVariables : dumped variable types, listed as following: +// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4), +// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8), +// -- heat flux of species diffusion term(Qs, 9), heat flux of vibrational temperature term(Qv, 10), heat flux of electron temperature term(Qe, 11), +// -- species mass fractions(Ns, 12), x component of wall velocity(Vx, 13), y component of wall velocity(Vy, 14), z component of wall velocity(Vz, 15), +// -- slip translational-rotational temperature(Tts, 16), slip vibrational temperature(Tvs, 17), slip electron temperature(Tes, 18), absolute wall velocity(Vs, 19), +// -- Stanton number(St, 20), coefficient of heat rate(Ch, 21), temperature jump(deltaT, 22), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24). +int nVisualVariables = 8; +int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15]; + +int nVisualWallVariables = 9; +int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11]; + +// dumpStandardModel: Dump many standard model data. +// 1 -- Turbulent flat plate. +int dumpStandardModel = 0; + +// ifSetDataMonitor: Whether to set the data monitor. +// 0 -- No. +// 1 -- Yes. +// dataMonitorType: The type of data Monitor. +// 0 -- Probes data monitor. +// 1 -- Lines data monitor. +// 2 -- Surfaces data monitor. +// probesDefineFile: Probes location information file. +// nLines: The number of lines need to be monitored. +// linesDefineFile: Lines location information file. +// nSurfaces: The number of surfaces need to be monitored. +// surfacesDefineFile: Surfaces location information file. +// searchCellsMethod: method to search the cell of each probe. +// 0 -- Nearest cell to the probe. +// 1 -- Real cell where the probe is located. +// nProbeVariables: Number of variables want to be dumped for probes monitered. +// probeVariables : Variable types dumped, listed as following: +// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6), +// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9), +// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12). +// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!! +// probeVariables order must from small to big. +// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables. +// 0 -- Take the value of probe's cell as probe real value. +// 1 -- Interpolation from probe's and neighbouring cell to probe. +// 2 -- Interpolation from probe's cell nodes to probe. +int ifSetDataMonitor = 0; + +int dataMonitorType = 0; +string probesDefineFile = "bin/probes_XYZ.dat"; + +//int dataMonitorType = 1; +//int nLines = 1; +//string linesDefineFile = "bin/lines_XYZ.dat"; + +//int dataMonitorType = 2; +//int nSurfaces = 4; +//string surfacesDefineFile = "bin/surfaces_XYZ.dat"; + +int searchCellsMethod = 0; + +int nProbeVariables = 14; +int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13]; +int probeVariablesInterpolationMethod = 0; + +#************************************************************************ +# Turbulence Parameter * +#************************************************************************ +// turbInterval: Iteration number of turbulence. +// kindOfTurbSource: Kinds of turbulent source. +// 0 -- Original. +// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0. +// transitionType: transition model type +// 0 -- none. +// 2 -- gama-re-theta. +// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition. +// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not. +int turbInterval = 1; +int turbOrderStruct = 2; +int kindOfTurbSource = 0; +int mod_turb_res = 0; +double freeStreamViscosity = 1.0e-3; +double muoo = 3.0; +double kwoo = 5.0; +int transitionType = 0; +double turbIntensity = -1.0; +int freeturbIntensitySRModify = 0; +double freeDecayXLocation = 0.0; +int compressibleCorrection = 0; +int transitionMaFix = 1; + +// maximum eddy viscosity (myt/my) max. +double eddyViscosityLimit = 1.0e10; +int monitor_vistmax = 0; + +#************************************************************************ +# LES Parameter * +#************************************************************************ +// iLES: Create LESSolver or not. +// = 1 -- Create LESSolver; +// != 1 -- not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 -- in only first sub-iter; +// != 0 -- in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 -- not; +// != 0 -- Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// sgsmodel: subgrid scale model. +// = "smagorinsky"; +// = "dsmCom"; +// = "wale"; +// = "sigma". +// deltaFunctionType: = 1 -- MAX(deltai, deltaj, deltak); +// = 2 -- pow(deltai * deltaj *deltak, 1/3); +// = 3 -- Devloped by Scotti. +// wallDampingFunctionType: = 0 -- no wall function; +// = 1 -- van Driest; +// = 2 -- developed by Dr. Deng Xiaobing; +// = 3 -- developed by Piomelli. +// turbViscousCutType: turbulent viscosity cut type. +// = 0 -- mu_total = mut + mul; +// = 1 -- mu_total = max(mut-mul, 0) + mul; +// = 2 -- mu_total = max(mut , 0) + mul. +// smagConstant: constant of smagorinsky model. +// waleConstant: constant of wale model. +// filterDirection [3]: filter variables in i, j, k direction or not. +// averageDirection[3]: average variables in i, j, k direction or not. +// isotropicConstant: constant of isotropic part of SGS stress. +int iLES = 0; +string sgsmodel = "smagorinsky"; +int deltaFunctionType = 2; +int wallDampingFunctionType = 1; +int turbViscousCutType = 2; +double smagConstant = 0.1; +double isotropicConstant = 0.0; +double waleConstant = 0.6; +double sigmaConstant = 1.35; +int filterDirection[] = [1, 1, 0]; +int averageDirection[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +#************************************************************************ +# Other Parameters for Hypersonic Non-equilibrium Gas * +#************************************************************************ +// dg_high_order: +// 0 -- generic order accuracy. +// 1 -- high order accuracy. +// iapplication: +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver, +// nm: Equation number of the physics, but is out of commision now. +// 4 -- for 2D. +// 5 -- for 3D. +// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas. +// Otherwise, the pure gas with one component is used for perfect gas. +// 0 -- Earth gas. +// 1 -- Mars gas. +// 2 -- Argon. +// 3 -- Nitrogen. +// nEnergyRecycle: The type of EnergyModel Recycle. +// 0 -- not used. +// 1 -- used. +// nDensityModify: The type of densitymodify. +// 0 -- not used. +// 1 -- used. +// nchem: +// 0 -- without chemical reaction flow. +// 1 -- the chemical reaction flow is considered. +// nEquilibriumGas: the variable is valid when the condition of nchem = 0 is satisfied. +// 0 -- perfect gas. +// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component. +// nPCWCycleStep: The maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition. +// The value equals to or is greater than 1, and 3 is for default value. +// nRETCycleStep: The maximum step number of iteration in the module of computing radiation equilibrium temperature on wall. +// The value equals to or is greater than 1, and 3 is for default value. +// nSLIPCycleStep:The maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction. +// The value equals to or is greater than 1, and 3 is for default value. +// nSlipBCModel: The computational model of slip boundary conditions. +// 0 -- no slip. +// 1 -- the conventional Maxwell slip conditions. +// 2 -- the Gokcen slip conditions. +// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al. +// 4 -- the Kogan simplified slip conditions. +// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested. +// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS). +// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter. +// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS). +// nchemsrc: +// 0 -- the source terms are not computed. +// 1 -- the source terms are computed. +// nchemrad: +// 0 -- compute the spectrum radius without considering chemical reaction flow. +// 1 -- compute the spectrum radius that need to count the contribution from chemical reaction flow. +// ntmodel: The thermodynamic temperature model. +// 1 -- One-temperature model. +// 2 -- Two-temperature model. +// 3 -- Three-temperature model. +// isUseNoneqCond: +// 0 -- compute the source terms without any conditions. +// 1 -- compute the source terms using the non-equilibrium condition. +// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value. +// nIdealState: whether take all gas species as ideal gas for gas-mixture process. +// 0 -- No. +// 1 -- Yes. // nTEnergyModel: the method to computing temperature energy model. +// 0 -- the energy term is computed using the conventional method. +// 1 -- the energy term is computed using the polynomial fitting method. +// 2 -- the energy term is computed using the piecewise polynomial fitting method. +// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model. +// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value. +// catalyticCoef: +// 0.0 -- full non-catalytic wall boundary condition. +// 1.0 -- full catalytic wall boundary condition. +// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient. +// nIsSuperCatalytic: the super catalytic condition for the fully catalytic wall, and assigned with the value of 1. +// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream. +// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components. +// nTemperatureJump: the method to calculate the temperature jump. +// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode. +// 1 -- the general method where the iteration is calculated with the translation-rotation temperature. +// nSurfGradMethod: the method to compute the surface heating ratio. +// 0 -- the gradient of variable is computed with the first-order difference method. +// 1 -- the gradient of variable is computed with the Green-Guass integral method. +// nRapidFlowfield: initialize the flowfield using the rapid engineering method when it is greater than zero. +// nSurfHeatMonitor: To exam the surface heating change or not. 0 is no, 1 is yes. +// nInitPressureStep: the steps to initialize the boundary variables when the rapid method is used. 100 is the default value. +// nDumpCFLNumber: 1 indicates dumping the CFL number to file, 0 denotes no dumping. +// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0]. +// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0]. +// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0]. +// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used. +// 1.0 -- proposed by Maxwell. +// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall. +// 1.146 -- proposed for an additional "fictitious" velocity slip. +// chemicalRelaxCorf: The value is in range of [0.001, 1.0]. +// spectrumRadiusCoef: The value is in range of [0.0, 2.0]. +// staticPressureRelaxCorf: The value is in range of [0.1, 1.0]. +// nIsChemicalFreeze: the flag to freeze the chemical reactions. +// 0 -- not freeze, the chemical reaction sources will be calculated. +// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated. +// veTemperatureMin: The minimum of Tv and Te. +// maxViscous: the maximum of Viscous. +// trTemperatureMin: the minimum value of trTemperature. +// veTemperatureMin: the minimum value of veTemperature. +// densityMin: the minimum value of density. +// tAdjustmentFactor: magnification of temperature, this value is in range of (1.0, 10.0]. +// nDebug: cout the Wrong place and abort +// 0 -- not used. +// 1 -- used. +// nSpeciesLimit: limitter of gas species +// 0 -- not used. +// 1 -- used. +// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction. +// 0 -- method 0. +// 1 -- method 1. +// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid. +// 0 -- not used. +// 1 -- used. +// nViscosityPeModified: Pe Modified for ViscosityCoef. +// 0 -- not used. +// 1 -- used. +// nChemcalSourceModified: Modified on ChemcalSource. +// 0 -- not used. +// 1 -- used. +// nChemcalSourceEsMethod: Modified on ChemcalSource. +// 0 -- approximation algorithm 1 (Ori). +// 1 -- approximation algorithm 2 (New). +// nMaxStepTemperature: the iterative steps of temperature. +// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs. +// 0 -- not used. +// 1 -- used. +// nDiagonalModified: Modified on Diagonal. +// 0 -- not used. +// 1 -- new. +// nDiagonalModifiedTurb: Modified on Diagonal for turbulence. +// 0 -- not used. +// 1 -- new. +// nGradPrimtiveMethod: +// 0 -- Ori. +// 1 -- new. +// nAblation: +// 0 -- The wall ablation is not computed. +// 1 -- The wall ablation is computed. +// isInjection: +// 0 -- The injection velocity of ablation wall is not computed. +// 1 -- The injection velocity of ablation wall is computed. +// nViscosityModel: +// 0 -- Blottner fitting method(N89). +// 1 -- Gupta fitting method(N90). +// nContinueModel: The new continue model can switch different computation model. +// 0 -- Not use the new continue model. +// 1 -- use the new continue model. +// nSutherland: +// 0 -- stands for selecting the Blotter curve fits mode. +// 1 -- stands for Sutherland relation. +// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11". +// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. +// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. +// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. +// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions. +// "Gas-Mixture" -- indicates the process of mixing gas without reacting. +// for struct solver mixing two species��SpeciesA, SpeciesB��. +// for unstruct solver mixing multi-species��O2 NO CO CO2 H2 N2 Air CH4��. +// For self-definition model, the gasfile is used to indicate the file path of the new gas model. +// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. +// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. +// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes. +// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation. +// nIterSecondStep: the maximum number of iteration in the second step for the self-adaptive calculation. +// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation. +// nEnergyAssembly: the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory. +// 0 -- no, +// 1 -- yes. +// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model. +// 0 -- the density. +// 1 -- the translation temperature. +// 2 -- the vibration temperature. +// 3 -- the electron temperature. +// 4 -- the pressure. +// 5 -- the mass fraction of oxygen. +// 6 -- the mass fraction of nitrogen. +// firstStepError : the residual error of the first step iteration for the self-adaptive calculation. +// secondStepError : the residual error of the second step iteration for the self-adaptive calculation. +// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation. +// nProtectData: Use the continuation file data protection mechanism. +// 0 -- no. +// 1 -- yes. +// nTvChange: Judge whether the Tv equals Ttr. +// 0 -- yes. +// 1 -- no. +// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions. +// nFraction: the initial fractions type of species. +// 0 -- mass fraction. +// 1 -- mole fraction. +int dg_high_order = 0; +int iapplication = 0; +int isAdaptiveSolver = 0; +int nm = 5; +int nEquilibriumGas = 0; +int nPCWCycleStep = 3; +int nRETCycleStep = 3; +int nSLIPCycleStep = 3; +int nIterFirstStep = 1000; +int nIterSecondStep= 2000; +int nIterThirdStep = 2000; +int nEnergyAssembly = 0; +int nControlVariable = 1; +double firstStepError = 0.01; +double secondStepError = 0.001; +double thirdStepError = 0.001; +double predictCFLError = 0.1; + +double refGama = 1.4; +double prl = 0.72; +double prt = 0.90; +double sc_l = 0.5; +double sc_t = 0.5; + +int nGasModel = 0; +int nchem = 0; +int nchemsrc = 1; +int nchemrad = 1; +int ntmodel = 1; + +int nIdealState = 0; +int nEnergyRecycle = 1; +int nSlipBCModel = 0; +int nDensityModify = 1; +int nTEnergyModel = 0; +int nMeanFreePathType = 0; +int nIsChemicalFreeze = 0; +int nIsSuperCatalytic = 1; +int nTemperatureJump = 0; +int nSurfGradMethod = 0; +int nRapidFlowfield = 0; +int nSurfHeatMonitor = 0; +int nInitPressureStep = 100; +int nDumpCFLNumber = 0; + +double parkVDPower = 0.6; +double catalyticCoef = 0.0; +double sigmaVelocity = 1.0; +double sigmaTemperature = 1.0; +double sigmaMassFraction = 1.0; +double velocitySlipCorrectConstant = 1.0; + +double chemicalRelaxCorf = 1.0; +double chemicalSpectrumRadiusCoef = 1.0; +double viscousSpectrumRadiusCoef = 1.5; +double inviscidSpectrumRadiusCoef = 1.5; +double spectrumRadiusCoef = 0.5; +double staticPressureRelaxCorf = 0.2; + +double maxViscous = 10000.0; +double trTemperatureMin = 10.0; +double veTemperatureMin = 30.0; +double maxTemperature = 50000.0; +double densityMin = 1.0e-8; +double densityMinFactor = 0.1; +double tAdjustmentFactor = 10.0; +double iniSpeedCoef = 1.0; +int iniSpeedMode = 0; + +int nDebug = 0; +int nSpeciesLimit = 1; +int nTurblenceForChemical = 0; +int nViscosityFluxSublevelModified = 1; +int nViscosityPeModified = 0; +int nChemcalSourceModified = 2; +int nChemcalSourceEsMethod = 1; +int nMaxStepTemperature = 5; +int veTemperatureMinModified = 1; +int nDiagonalModified = 0; +int nDiagonalModifiedTurb = 0; +int nGradPrimtiveMethod = 1; +int nInviscidFluxModify = 1; +int nQlLimitMethod = 2; +int nSpeciesForWallMethod = 1; +int nDensityForWallMethod = 0; +int wallMultiTemperature = 0; + +int nProtectData = 0; +int nAblation = 0; +int isInjection = 0; +int nViscosityModel = 0; +int nMarsModel = 0; +int nTvChange = 0; +int isMoleFractionType = 0; +string gasfile = "DK5"; +//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat"; +string speciesName = "O, O2, NO, N, N2"; +string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767"; + +//string speciesName = "O, O2, NO, N, NO+, N2, e-"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 0.0"; + +//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0"; + +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + +//string gasfile = "Pa"; +//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0"; + +//string gasfile = "Combustion-12"; +//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2"; +//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767"; + +//string gasfile = "Gas-Mixture"; +//string speciesName = "SpeciesA, SpeciesB"; +//string initMassFraction = "1.0, 0.0"; +int nSutherland = 0; +double gamaSpeciesA = 1.4; +double gamaSpeciesB = 1.3; +double molecularWeightSpeciesA = 29.0; +double molecularWeightSpeciesB = 30.0; + +//string gasfile = "Gas-Mixture"; +//string speciesName = "O2, N2"; +//string initMassFraction = "1.0, 0.0"; + +int nFraction = 0; +int nContinueModel = 0; +int nChemicalFlowStep = 0; +int ifStartFromPerfectGasResults = 0; +int isUseNoneqCond = 0; +double frozenCondition = 0.01; + +int nLeakageMonitor = 0; +double totalLeakageVolume = 1000.0; +double monitorThresholdValue = 0.05; +double sprayFactor = 0.0; + +######################################################################### +// Multi-Grid parameters. +// nMGLevel: The number of level of Multi-Grid. +// <= 1 -- Single-level. +// > 1 -- multi-level. +// MGPreIteration: For each grid, the number of pre-smoothing steps. +// n_post: For each grid, the number of post-smoothing steps. +// MGCoarsestIteration: For the coarest grid the number of smoothing steps. +// MGFasType: V-multi cycle or W-multi cycle. +// 1 -- V-multi cycle. +// 2 -- W-multi cycle. +// flowInitStep: Flow initialization step, 0 - 500 is suggested. +// Multi-Grid : Number of steps computing on coarse grid, during flow initialization. +// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization. +// mgCFLScale: CFL number enlarge times for coarse grid. +// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid. +// 1 -- zero order. +// 2 -- first-order. (default) +// mgCorrectionLimit: Multi-grid correction limit. +int nMGLevel = 1; +int MGCoarsestIteration = 1; +int MGPreIteration = 1; +int MGFasType = 1; +int n_post = 0; +int flowInitStep = 100; +int mprol = 2; +double mgCFLScale = 1.0; +double mgCorrectionLimit = 0.01; + +//--------------- Some parameter for turbulent model -------------------- +// neasm: The variation of kw turbulent model. +// ismooth_turb: Residual smooth for turb or not. +// SSTProductType: The type of product term based on vorticity for SST. +// SAProductType: The type of product term based on vorticity for SA. +int neasm = -3; +int SSTProductType = 0; +int ismooth_turb = 0; +int SAProductType = 2; + +// ----------------- Overset Grid parameter ----------------------------- +int codeOfDigHoles = 1; +int codeOfTurbulentModel = 0; +string masterFileName = "./grid/searchFile.inp"; +string holeBasicFileName = "./grid/holeBasicFile.inp"; +string holeFullFileName = "./grid/holeFullFile.dat"; +string linkFileName = "./grid/topology.dat"; +string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; + +#************************************************************************ +# High Order Struct Solver * +#************************************************************************ +// isFVMOrFDM: +// 0 -- NSSolverStruct using Finite Volume Method. +// 1 -- NSSolverStruct using Finite Differ Method. +// SolverStructOrder: Spatial discretisation order of NS equations with struct grid. +// <= 2 -- finite volume method. +// >= 3 -- finite difference order. (to be completed) +// 0 -- default. +// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence, +// smaller epsilon, robuster for shock-detecting. +// str_highorder_interpolation_type: +// -- "classical", "test". +// str_highorder_flux_name: +// -- "roe", "steger". +// structhighordergradient: +// -- "conservation", "chain_rule". +int isFVMOrFDM = 0; +string str_highorder_solver = "WCNS"; +int SolverStructOrder = 0; +double str_highorder_interpolation_epsilon = 1.0e-6; +string str_highorder_interpolation_type = "test"; +string str_highorder_flux_name = "steger"; +string structhighordergradient = "conservation"; +double coefofstrflux = 0.5; +double limitcoefofinterface = 0.0; + +// ----------------- Advanced choices ----------------------------------- +// outtimesc: Time stepping scheme for the outer loop. +// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1]. +// -1 -- seconde-order fully-upwind differencing. +// 0 -- seconde-order upwind-biased differencing. +// 0.333333 -- third-order upwind-biased differencing. +// 1 -- seconde-order central differencing. +// MUSCLCoefXb: The limiter parameter. +// 0 -- the effect of the limiter is cancelled, means the first-order interpolations. +// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1. +string outtimesc = "impbd2"; +double MUSCLCoefXk = -1; +double MUSCLCoefXb = 1.0; +int allReduceStep = 1; + +// ----------------- overlap configuration ------------------------------ +// codeOfOversetGrid: Overlapping(overset) grid or not. +// 0 -- NON-overlapping grid. +// 1 -- Overlapping grid. +// oversetInterpolationMethod: the method of overset interpolation while field simulation. +// 0 -- set the acceptor cell value by donor cell value. +// 1 -- set the acceptor cell value by distance weight of donor cell value. +// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated. +// 0 -- no. +// 1 -- yes. +// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in +// the current overset grid(only for three dimension). +// 0 -- no. +// 1 -- yes. +// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid. +// 0 -- no. +// 1 -- yes. +// walldistMainZone: The initial value of background grid which does not exist wall boundary condition. +// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell. +// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region. +// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary. +// 0 -- one layer. +// 1 -- two layers. +// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region. +// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure. +// 0 -- no. +// 1 -- yes. +int codeOfOversetGrid = 0; +int oversetInterpolationMethod = 0; +int readOversetFileOrNot = 0; +int symetryOrNot = 0; +int readInAuxiliaryInnerGrid = 0; +int readInAuxiliaryOuterGrid = 0; +int readInSklFileOrNot = 0; +string auxiliaryInnerGrid0 = "./grid/aux-upper.fts"; +string auxiliaryInnerGrid1 = "./grid/aux-lower.fts"; +string auxiliaryInnerGrid2 = ""; +string oversetGridFileName = "./grid/iblank.ovs"; +double walldistMainZone = 1.0 +double toleranceForOversetSearch = 1.0e-3; +double toleranceForOversetBox = 1.0e-3; +int twoOrderInterpolationOrNot = 0; +int keyEnlargeOfActiveNodes = 0; +int outTecplotOverset = 0; +int outPutOversetVisualization = 0; +int numberOfMovingBodies = 2; + +// ----------------- ALE configuration ------------------------------ +int codeOfAleModel = 0; +int aleStartStrategy = -1; + +double referenceLength = 1.0; +double referenceVelocity = 1.0; +double referenceDensity = 1.0; + +int strategyForFaceNormalVelocity = 0; // 0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd. +int strategyForGCLSource = 0; // 0-present; 1-Ahn. + +// 0: 1st-Admas-Bashforth; 1: 2nd-Admas-Bashforth; 2: 1st-Implicit-Euler; 3: 2nd-Implicit Euler; 4: 2nd-Adams-Moulton; 5: 3rd-Adams-Moulton. +int methodForKineticEquation = 0; +double relaxParameterOfKinetic = 1.0; + +#************************************************************************ +# motive information * +#************************************************************************ +int numberOfMovingBodies = 1; + +############################## body0 ############################## +// mass of parts. +double mass_0 = 1.0; +// gravity of parts (along negative direction in Y-axis, eg. 9.8). +double gravity_0 = 0.0; +// mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz. +double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0; +// initial six DOF position information of parts. xc yc zc. +double massCenter_0[] = 0.0, 0.0, 0.0; +// if reset mass center while restart. +int resetMassCenter_0 = 0; +// position offset of parts. dx dy dz. +double massCenterDxyz_0[] = 0.0, 0.0, 0.0; +// initial six DOF position information of parts. angleX angleY angleZ. +double attitudeAngle_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. vc vy vz. +double massCenterVelocity_0[] = 0.0, 0.0, 0.0; +// initial six DOF move information of parts. omigX omigY omigZ. +double angularVelocity_0[] = 0.0, 0.0, 0.0; +// the object that the parts belong to. +int fartherIndex_0 = -1; +// the assembly position of the parts. xc yc zc angleX angleY angleZ. +double configPamameter_0[] = 0.0, 0.0, 0.0, 0.0, 0.0, 0.0; +// the move pattern of the parts. +// -1 given motion partten. +// 0 still. +// 1 six DOF motion. +// 2 three DOF motion. +// 11 X-axis forced motion. +// 12 Y-axis forced motion. +// 13 Z-axis forced motion. +// 14 forced pitch motion. +// 15 forced yaw motion. +// 16 forced roll motion. +int RBDMethod_0 = 0; +double amplitude_0 = 0.0; +double reduceFrequency_0 = 0.0; +// direction of rotation. +// 1 -- clockwise from the point of view along the positive x axis. +// -1 -- anticlockwise from the point of view along the positive x axis. +int direction_0 = -1; +double rotateFrequency_0 = 0.0; +//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter"; +// dimensional physical time for additional force(s). +double addedForceTime_0[] = 0.0; +// additional force(inertia system) fX fY fZ. +double addedForce_0[] = 0.0, 0.0, 0.0; +// additional moment(inertia system) mX mY mZ. +double addedMoment_0[] = 0.0, 0.0, 0.0; +// the deformation method of the parts. +int morphing_0 = 0; + +// post indentify. +int integralOrder = 4; + +// ---------------- ATP read -------------------------------------------- +//@int inflowParaType = 0; +//@double refReNumber = 6.5e6; +//@double refDimensionalTemperature = 288.15; +//@double freestream_vibration_temperature = 300.00; +//@double refDimensionalPressure = 0; +//@double height = 0; +//@int nsubsonicInlet = 0; +//@int nsubsonicOutlet = 0; +//@string inLetFileName = "./bin/subsonicInlet.hypara"; +//@string outLetFileName = "./bin/subsonicOutlet.hypara"; +//@double refDimensionalVelocity = 0; +//@double refDimensionalDensity = 0; +//@string weatherDataFilePath = "./WRFData/"; +//@double longitude = 110.95 +//@double latitude = 19.61; +#************************************************************************ +# Old Parameter * +#************************************************************************ +int isPlotVolumeField = 0; + +#************************************************************************ +# partial flow field setting Parameter * +#************************************************************************ +//int nPartialParameter = 0; // 0/1/2 +//int nNumberOfPartialField = 0; // +//int nStartGridIndex[] = [0]; +//int nEndGridIndex[] = [0]; + +//double partialCFL[] = [0.0]; +//double partialSpeedCoef[] = [0.0]; +//double partialSpeed[] = [0.0]; +//double partialAttackd[] = [0.0]; +//double partialSlide[] = [0.0]; +//double partialPressure[] = [0.0]; +//double partialTemperature[] = [0.0]; +//double partialMassFractions[] = [0.0]; + +#************************************************************************ +# Incompressible Parameter * +#************************************************************************ +int isSolveEnergyEquation = 0; +int isSolveTurbEquation = 0; +int isSolveSpeciesEquation = 0; \ No newline at end of file diff --git a/L06_TwoD_Spoiler_BGK_OMP_4CPU/bin/input.txt b/L06_TwoD_Spoiler_BGK_OMP_4CPU/bin/input.txt new file mode 100644 index 0000000..ba067cb --- /dev/null +++ b/L06_TwoD_Spoiler_BGK_OMP_4CPU/bin/input.txt @@ -0,0 +1,33 @@ +0 ！MRT set 1, BGK set 0 +0 ic.plt ！CONTI, resume :1 , new 0 //follows input datafile name +0 ！LES yes: 1 , no: 0 +1 mesh_2d.dat ！GEO read complex geo? yes:1, no:0 //follows input datafile name +1 ! MB multiblock LBM? yes:1, no:0 +0 2.e-3 !CONV using converge criterion? yes:1, no:0 +600 ！NX +400 ! NY +1 ! NZ +240 ！ NX2 +160 ！ NY2 +1 ! NZ2 +200 ! LowX +160 ! LowY +0 ! LowZ +200 ! framerate +50000 ！total steps to terminate +1.0 ! density +0.54 ！ tau +(0.0, 0.0, 0.0000000) ！ Volumetric force vector (gx, gy, gz) +D2Q9 ! velocity set +Poiseuille ! boundary condition +! note: in the following, boundary types: periodic,velocity, pressure +! are allowed. if "velocity" is applied, please strictly follow the format "velocity (%lf, %lf, %lf)". +velocity (0.1, 0.00, 0.0) ！xmin face +pressure 1.0 ！xmax face +velocity (0.1, 0.00, 0.0) ！ymin face +velocity (0.1, 0.00, 0.0) ！ymax face, +nonslip ！zmin face +nonslip ！zmax face +-------------------！ initial velocity field +(0.1, 0.00, 0.0) + diff --git a/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/key.hypara b/L06_TwoD_Spoiler_BGK_OMP_4CPU/bin/key.hypara similarity index 91% rename from H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/key.hypara rename to L06_TwoD_Spoiler_BGK_OMP_4CPU/bin/key.hypara index 9c32184..c267e0a 100644 --- a/H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU/bin/key.hypara +++ b/L06_TwoD_Spoiler_BGK_OMP_4CPU/bin/key.hypara @@ -17,12 +17,12 @@ string defaultParaFile = "./bin/cfd_para.hypara"; int ndim = 2; int nparafile = 1; -int nsimutask = 0; -string parafilename = "./bin/cfd_para_incompressible.hypara" +//int nsimutask = 0; //string parafilename = "./bin/cfd_para_subsonic.hypara"; //string parafilename = "./bin/cfd_para_transonic.hypara"; //string parafilename = "./bin/cfd_para_supersonic.hypara"; //string parafilename = "./bin/cfd_para_hypersonic.hypara"; +//string parafilename = "./bin/cfd_para_incompressible.hypara"; //int nsimutask = 1; //string parafilename = "./bin/grid_para.hypara"; @@ -39,6 +39,9 @@ string parafilename = "./bin/cfd_para_incompressible.hypara" //int nsimutask = 1; //string parafilename = "./bin/grid_refine_para.hypara"; +int nsimutask = 17; +string parafilename = "./bin/cfd_para.hypara"; + //int nsimutask = 14; //string parafilename = 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