455 lines
12 KiB
C++
455 lines
12 KiB
C++
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
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// PPPPP H H EEEEE N N GGGGG L EEEEE III +
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// P P H H E NN N G L E I +
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// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
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// P H H E N N N G G L E I +
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// P H H EEEEE N N GGGGG LLLLL EEEEE III +
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//------------------------------------------------------------------------+
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// Platform for Hybrid Engineering Simulation of Flows +
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// China Aerodynamics Research and Development Center +
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// (C) Copyright, Since 2010 +
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//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
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//! @file Constants.h
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//! @brief Define some global const value.
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//! @author He Xin.
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#pragma once
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#include "Precision.h"
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namespace PHSPACE
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{
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const int SOLVER_BASED = 0;
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const int GRID_BASED = 1;
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const int DENSITY_BASED_SOLVER = 0;
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const int PRESSURE_BASED_SOLVER = 1;
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const int FV_METHOD = 0;
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const int FD_METHOD = 1;
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const int SOLVE_FIELD = 0;
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const int CREATE_GRID = 1;
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const int CAL_WALL_DIST = 2;
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const int PARTITION_GRID = 3;
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const int REPOSITORY = 4; //! Useless.
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const int OVERSETGRID_VIEW = 5;
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const int OVERSET_CONFIG = 6;
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const int CONVERT_PARTITION = 7;
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const int DSMC_SOLVER = 8; //! Useless.
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const int HELICOPTER = 9; //! Useless.
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const int UGKS_SOLVER = 10; //! Useless.
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const int HO_SOLVER = 12;
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const int LBM_SOLVER_MPI = 13;
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const int LBM_SOLVER_OMP = 17;
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const int INTEGRATIVE_SOLVER = 14;
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const int GRIDCHECK_SOLVER = 15;
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const int GRID_SOLVER = 16;
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const int SPECDIFFHYB_SOLVER = 51;
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const int SPEC_SOLVER = 52;
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const int DERIVATIVE_IDENITFY = 98;
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const int POST_PROCESSING = 99;
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const int NOLES_SOLVER = 0;
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const int LES_SOLVER = 1;
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const int GRID_CONVERSION = 1;
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const int GRID_REFINE = 2;
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const int GRID_MERGING = 3;
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const int GRID_DEFORMATION = 4;
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const int GRID_REPAIR = 5;
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const int GRID_MIRROR = 6;
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const int GRID_STRTOUNS = 7;
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//! Type of rotating reference frame.
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const int STATIONARY_FRAME = 0;
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const int TRANSLATIONAL_FRAME = 1;
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const int ROTATIONAL_FRAME = 2;
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//! periodicType
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const int NO_PERIODICITY = 0;
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const int TRANSLATIONAL_PERIODICITY = 1;
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const int ROTATIONAL_PERIODICITY = 2;
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const RDouble half = 0.5;
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const RDouble third = 1.0 / 3.0;
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const RDouble two3rd = 2.0 / 3.0;
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const RDouble four3rd = 4.0 / 3.0;
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const RDouble fourth = 0.25;
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const RDouble sixth = 1.0 / 6.0;
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const RDouble eighth = 1.0 / 8.0;
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const RDouble tenth = 0.1;
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const RDouble zero = 0.0;
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const RDouble one = 1.0;
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const RDouble two = 2.0;
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const RDouble three = 3.0;
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const RDouble four = 4.0;
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const RDouble five = 5.0;
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const RDouble six = 6.0;
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const RDouble seven = 7.0;
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const RDouble eight = 8.0;
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const RDouble nine = 9.0;
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const RDouble ten = 10.0;
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const RDouble eleven = 11.0;
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const RDouble twelve = 12.0;
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const RDouble thirteen = 13.0;
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const RDouble fourteen = 14.0;
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const RDouble fifteen = 15.0;
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const RDouble sixteen = 16.0;
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const RDouble seventeen = 17.0;
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const RDouble eighteen = 18.0;
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const RDouble nineteen = 19.0;
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const RDouble twenty = 20.0;
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const RDouble PI = 3.141592653589793;
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const RDouble straightAngle = 180.0;
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const int SEGCTION_LENGTH = 10240;
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const int NS_EQUATION = 1;
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const int TURBULENCE = 2;
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const int TRANSITION = 3;
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const int NONDIMENSIONCONDITION = 0;
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const int FLIGHTCONDITION = 1;
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const int EXPERIMENTCONDITION = 2;
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const int SUBSONICBCCONDITION = 3; //! Useless.
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const int TEMPERATURE_DENSITY = 4;
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const int TEMPERATURE_PRESSURE = 5;
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const int MACH_TEMP_PRE = 6;
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const int WEATHERCONDITION = 7;
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const int PRIMITIVE_VARIABLES = 9;
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const int TRAJECTORY = 10;
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const int VIS_STD = 0;
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const int VIS_AVER = 1;
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const int VIS_TEST = 2;
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const int VIS_NEW1 = 3;
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const int VIS_NEW2 = 4;
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const int VIS_ERIC = 5;
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const int ISCHEME_ROE = 1;
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const int ISCHEME_VANLEER = 2;
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const int ISCHEME_STEGER = 3;
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const int ISCHEME_HLLE = 4;
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const int ISCHEME_LAX_FRIEDRICHS = 5;
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const int ISCHEME_AUSM = 6;
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const int ISCHEME_AUSMP = 7;
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const int ISCHEME_AUSMPUP = 8;
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const int ISCHEME_AUSMDV = 9;
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const int ISCHEME_AUSM_W = 10;
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const int ISCHEME_AUSMPW = 11;
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const int ISCHEME_Rotate = 12;
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const int ISCHEME_ROE_MODIFIED = 13;
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const int ISCHEME_AUSMPW_PLUS = 14;
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const int ISCHEME_GMRES_ROE = 15; //! GMRES modified Roe scheme for assembling Jacobian matrix using FD
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const int ISCHEME_GMRES_Steger = 16; //! GMRES modified Steger scheme GMRES3D
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const int FIRST_ORDER = 1;
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const int SECOND_ORDER = 2;
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const int ILMT_NOLIM = 1;
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const int ILMT_FIRST = 2;
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const int ILMT_BARTH = 3;
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const int ILMT_VENCAT = 4;
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const int ILMT_STRUCT = 10;
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const int ILMT_MINMOD = 11;
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const int ILMT_VAN_ALBADA = 12;
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const int ILMT_VAN_ALBADA_CLZ = 13;
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const int ILMT_VANLEER = 14;
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const int ILMT_SMOOTH = 15;
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const int ILMT_MINMODTEST = 16;
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const int ILMT_MIN_VAN = 17;
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const int ILMT_3rd_SMOOTH = 18;
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const int ILMT_3rd_Minmod_SMOOTH = 19;
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const int ILMT_WENO3_JS = 20;
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const int ILMT_WENN3_PRM211 = 21;
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const int ILMT_WENN3_ZM = 22;
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const int ILMT_WENN3_ZES2 = 23;
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const int ILMT_WENN3_ZES3 = 24;
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const int INVISCID = 0;
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const int LAMINAR = 1;
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const int ALGEBRAIC = 2;
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const int ONE_EQU = 3;
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const int TWO_EQU = 4;
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const int IREGAMA = 2;
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const int BALDWIN_LOMAX = 10;
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const int SPALART_ALLMARAS = 11;
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const int KW_SST = 12;
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const int KEPSILON = 13;
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const int INCOMPRESSIBLE = 0;
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const int COMPRESSIBLE = 1;
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const int MULTI_STAGE = 1;
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const int LU_SGS = 4;
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const int Block_LU_SGS = 5;
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const int JACOBIAN_ITERATION = 6;
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const int Line_LU_SGS = 7;
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const int Matrix_LU_SGS = 8;
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const int GMRES = 9;
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const int OneRefineOneDeform = 1;
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const int DeformAfterAllRefine = 2;
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const int X_DIR = 1;
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const int Y_DIR = 2;
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const int Z_DIR = 3;
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const int PHINT = 1;
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const int PHFLOAT = 2;
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const int PHDOUBLE = 3;
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const int PHSTRING = 4;
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const int PHBOOL = 5;
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const RDouble SAME_POINT_TOL = static_cast<RDouble> (1.0e-12);
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const int PROBESMONITOR = 0;
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const int LINESMONITOR = 1;
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const int SURFACESMONITOR = 2;
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const int NEARESTCELLDATA = 0;
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const int REALCELLDATA = 1;
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const int CELLVALUE = 0;
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const int CELLSTOPROBE = 1;
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const int NODESTOPROBE = 2;
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const int NON_GHOST = 0; //! These are interior cells.
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const int ONE_GHOST_LAYER = 1; //! Their have one-layer ghost cells.
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const int TWO_GHOST_LAYER = 2; //! Their have two-layer ghost cells.
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const int THREE_GHOST_LAYER = 3; //! Their have three-layer ghost cells.
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const int GlobalCoordinate = 0;
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const int LocalCoordinate = 1;
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namespace IDX
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{
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const int IR = 0;
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const int IU = 1;
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const int IV = 2;
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const int IW = 3;
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const int IP = 4;
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const int IRU = 1;
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const int IRV = 2;
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const int IRW = 3;
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const int IRE = 4;
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const int IA = 0;
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const int IX = 1;
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const int IY = 2;
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const int IZ = 3;
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const int IKES = 1;
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const int IETA = 2;
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const int IZTA = 3;
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const int ISA = 0;
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const int IKE = 0;
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const int IKW = 1;
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const int IGAMA = 0;
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const int IRECT = 1;
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const int ITT = 0;
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const int ITV = 1;
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const int ITE = 2;
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// these variables are for SIMPLE algorithm.
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const int S_IU = 0;
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const int S_IV = 1;
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const int S_IW = 2;
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const int S_IP = 3;
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const int S_IR = 4;
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const int S_ITEMP = 5;
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const int S_ITURBK = 6;
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const int S_IEPSILON = 7;
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const int S_IOMEGA = 8;
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const int S_ISA = 9;
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const int S_IEDDYVISC = 10;
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const int S_IAIR = 15;
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const int S_IH2 = 16;
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const int S_IH2_l = 17;
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const int S_INH3_l = 18;
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const int S_ICH4 = 19;
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const int S_IC2H4 = 20;
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const int S_IC3H8 = 21;
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const int S_ING = 22;
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const int S_ILNG = 23;
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const int S_IH2S = 24;
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const int S_ICl2 = 25;
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const int S_INH3 = 26;
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const int S_IC2H6 = 27;
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const int MOMX_EQ = 0;
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const int MOMY_EQ = 1;
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const int MOMZ_EQ = 2;
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const int CONT_EQ = 3;
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const int ENER_EQ = 4;
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const int ZNUT_EQ = 5;
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const int TURBK_EQ = 6;
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const int EPSILON_EQ = 7;
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const int OMEGA_EQ = 8;
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}
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const int MAX_SPECIES_NUM = 20; //! The maximum number of species.
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const int MAX_REACTION_NUM = 50; //! The maximum number of reactions.
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namespace WALLFUNCTION
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{
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const int NONE = 0;
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const int STANDARD = 1;
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const int PAB3D = 2;
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}
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namespace ABLATION
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{
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const RDouble FormationHeat = 13.083E+07;
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}
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#define BOLTZMANN_CONSTANT 1.380649E-23 //! The Boltzmann constant, Unit: J/K.
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#define AVOGADRO_CONSTANT 6.0225E+23 //! The Avogadro constant, Unit: mol-1.
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#define VACUUM_PERMITTIVITY 8.854187817E-12 //! The permittivity of vacuum,Unit: C/(V*m).
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#define STANDARD_PRESSURE 101325.0 //! The standard atmosphere pressure,Unit: Pa.
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#define ELECTRIC_QUANTITY 1.602176634E-19 //! The electric quantity, Unit: C.
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#define GeneralGasConstant 8.31434 //! The general gas constant, J/(kg * K).
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}
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//---------------------------
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// Pressure-based enum
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//----------------------------
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typedef enum
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{
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Projection = 1,
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SIMPLE = 2,
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SIMPLEC = 3,
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PISO = 4
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}InCom_method;
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typedef enum
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{
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HYPRELib = 0,
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UNAPLib = 1,
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YHAMGLib = 2
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}mathLibName;
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typedef enum
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{
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GaussSeidelMethod = 0,
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GMRESMethod = 1,
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BicgstabMethod = 2,
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AMGMethod = 3,
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PCGMethod = 4,
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FlexGMRESMethod = 5,
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LGMRESMethod = 6,
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COGMRESMethod = 7,
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CGNRMethod = 8,
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MGRMethod = 9,
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ILUMethod = 10,
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AMGDDMethod = 11,
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HybridMethod = 12,
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PipeBicgstabMethod = 13,
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PipeCGMethod = 14,
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PipeGMRESMethod = 15
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}LinearSolverID;
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typedef enum
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{
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L1Res = 1,
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L2Res = 2,
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LinfRes = 3,
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}ResidualID;
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typedef enum
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{
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iNone = 0,
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iILU = 1,
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iAMG = 2,
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iEuclid = 3,
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DiagScale = 4,
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PILUT = 5,
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GSMG = 6,
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ParaSails = 7,
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LduDiag = 8,
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LduDIC = 9,
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LduDILU = 10,
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LduBJacobi = 11,
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iBJILU = 12,
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iBJSOR = 13,
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iJacobi = 14,
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iSOR = 15,
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iAMGDD = 16
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}PrecondTypeID;
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typedef enum
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{
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None = 0,
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MinimumCorrection = 1,
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OrthogonalCorrection = 2,
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OverrelaxedCorrection = 3
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} InCom_nonOrthMethod;
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typedef enum
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{
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firstUpWind = 0,
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secondUpWind = 1,
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QUICKMTHOD = 2,
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SecondCentral = 3,
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} invFluxScheme;
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typedef enum
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{
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iDefScheme = 0,
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iCentralScalar = 1,
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iCentralScalarReconst = 5,
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iCentralMatrix = 2,
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iUpwindAUSMPlus = 3,
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iUpwindRoe = 4
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}SpaceScheme;
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typedef enum
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{
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iEuler = 0,
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iNSLam = 1,
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iSAWallF = 2,
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iKEStandard = 3,
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iSSTWallF = 4
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}Model;
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typedef enum
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{
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WriteBoundary,
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WriteBlock,
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Writecomplete
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} plotFieldType;
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typedef enum
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{
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Tecplot_Binary,
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Tecplot_ASCII,
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Ensight_Binary,
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Ensight_ASCII
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} VisualfileType;
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namespace TEC_SPACE
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{
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const int ORDERED = 0;
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const int FELINESEG = 1;
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const int FETRIANGLE = 2;
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const int FEQUADRILATERAL = 3;
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const int FETETRAHEDRON = 4;
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const int FEBRICK = 5;
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const int FEPOLYGON = 6;
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const int FEPOLYHEDRON = 7;
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const int BoundaryVisual = 0;
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const int FieldVisual = 1;
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const int BlockVisual = 2;
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}
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