forked from p35462178/gks2d-str
373 lines
9.6 KiB
C++
373 lines
9.6 KiB
C++
#include"boundary_layer.h"
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void boundary_layer()
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{
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Runtime runtime;
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runtime.start_initial = clock();
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Block2d block;
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block.uniform = false;
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block.ghost = 3;
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double tstop = 20000;
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block.CFL = 0.3;
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K = 3;
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Gamma = 1.4;
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Pr = 1.0;
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double renum = 1e5;
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double den_ref = 1.0;
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double u_ref = 0.15;
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double L = 100;
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//prepare the boundary condtion function
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Fluid2d* bcvalue = new Fluid2d[1];
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bcvalue[0].primvar[0] = den_ref;
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bcvalue[0].primvar[1] = u_ref;
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bcvalue[0].primvar[2] = 0.0;
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bcvalue[0].primvar[3] = den_ref / Gamma;
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Mu = den_ref * u_ref * L / renum;
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cout << Mu << endl;
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//prepare the reconstruction function
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gausspoint = 1;
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SetGuassPoint();
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reconstruction_variable = conservative;
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wenotype = wenoz;//只有WENO才会起作用
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cellreconstruction_2D_normal = Vanleer_normal;
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cellreconstruction_2D_tangent = Vanleer_tangent;
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g0reconstruction_2D_normal = Center_3rd_normal;
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g0reconstruction_2D_tangent = Center_3rd_tangent;
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is_reduce_order_warning = true;
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flux_function_2d = GKS2D;
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gks2dsolver = gks2nd_2d;
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tau_type = NS;
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c1_euler = 0.0;
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c2_euler = 0;
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timecoe_list_2d = S1O2_2D;
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Initial_stages(block);
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Fluid2d* fluids = NULL;
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Interface2d* xinterfaces = NULL;
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Interface2d* yinterfaces = NULL;
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Flux2d_gauss** xfluxes = NULL;
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Flux2d_gauss** yfluxes = NULL;
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//读入2维结构化网格，先找到网格名字
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string grid = add_mesh_directory_modify_for_linux()
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+ "structured-mesh/flat-plate-str.plt";
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//读入2维结构化网格，格式是tecplot的3维binary，z方向只有一层。可以通过pointwise输出tecplot的binary格式实现
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Read_structured_mesh
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(grid, &fluids, &xinterfaces, &yinterfaces, &xfluxes, &yfluxes, block);
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ICfor_uniform_2d(fluids, bcvalue[0].primvar, block);
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runtime.finish_initial = clock();
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block.t = 0;
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block.step = 0;
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int inputstep = 1;
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while (block.t < tstop)
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{
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if (block.step % inputstep == 0)
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{
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cout << "pls cin interation step, if input is 0, then the program will exit " << endl;
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cin >> inputstep;
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if (inputstep == 0)
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{
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output2d(fluids, block);
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break;
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}
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}
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if (runtime.start_compute == 0.0)
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{
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runtime.start_compute = clock();
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cout << "runtime-start " << endl;
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}
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CopyFluid_new_to_old(fluids, block);
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block.dt = Get_CFL(block, fluids, tstop);
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for (int i = 0; i < block.stages; i++)
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{
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boundaryforBoundary_layer(fluids, block, bcvalue[0]);
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Convar_to_Primvar(fluids, block);
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Reconstruction_within_cell(xinterfaces, yinterfaces, fluids, block);
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Reconstruction_forg0(xinterfaces, yinterfaces, fluids, block);
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Calculate_flux(xfluxes, yfluxes, xinterfaces, yinterfaces, block, i);
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Update(fluids, xfluxes, yfluxes, block, i);
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}
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++block.step;
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block.t = block.t + block.dt;
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if (block.step % 100 == 0)
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{
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cout << "step 10 time is " << (double)(clock() - runtime.start_compute) / CLOCKS_PER_SEC << endl;
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}
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Residual2d(fluids, block, 10);
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output_wall_info_boundary_layer(xinterfaces, yinterfaces, xfluxes, yfluxes, block, L);
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output_skin_friction_boundary_layer(fluids, yinterfaces, yfluxes, block, u_ref, renum, L);
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if (block.step % 5000 == 0 || abs(block.t - tstop) < 1e-14)
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{
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output2d(fluids, block);
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char loc1[] = "0050";
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char loc2[] = "0105";
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char loc3[] = "0165";
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char loc4[] = "0265";
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char loc5[] = "0305";
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char loc6[] = "0365";
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char loc7[] = "0465";
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output_boundary_layer(fluids, block, bcvalue[0].primvar, 0.050 * L, loc1);
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output_boundary_layer(fluids, block, bcvalue[0].primvar, 0.105 * L, loc2);
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output_boundary_layer(fluids, block, bcvalue[0].primvar, 0.165 * L, loc3);
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output_boundary_layer(fluids, block, bcvalue[0].primvar, 0.265 * L, loc4);
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output_boundary_layer(fluids, block, bcvalue[0].primvar, 0.305 * L, loc5);
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output_boundary_layer(fluids, block, bcvalue[0].primvar, 0.365 * L, loc6);
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output_boundary_layer(fluids, block, bcvalue[0].primvar, 0.465 * L, loc7);
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}
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}
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runtime.finish_compute = clock();
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;
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cout << "\n the total running time is " << (double)(runtime.finish_compute - runtime.start_initial) / CLOCKS_PER_SEC << "秒！" << endl;
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cout << "\n the time for initializing is " << (double)(runtime.finish_initial - runtime.start_initial) / CLOCKS_PER_SEC << "秒！" << endl;
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cout << "\n the time for computing is " << (double)(runtime.finish_compute - runtime.start_compute) / CLOCKS_PER_SEC << "秒！" << endl;
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}
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void boundaryforBoundary_layer(Fluid2d* fluids, Block2d block, Fluid2d bcvalue)
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{
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inflow_boundary_left(fluids, block, bcvalue);
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inflow_boundary_right(fluids, block, bcvalue);
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//free_boundary_up(fluids, block, bcvalue);
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//outflow_boundary_up(fluids, block, bcvalue);
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inflow_boundary_up(fluids, block, bcvalue);
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//the boundary at the bottom
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int order = block.ghost;
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for (int j = order - 1; j >= 0; j--)
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{
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for (int i = order; i < block.nx; i++)
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{
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int index = i * block.ny + j;
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int ref = i * block.ny + 2 * order - 1 - j;
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if (fluids[index].coordx < 0.0)
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{
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fluids[index].convar[0] = fluids[ref].convar[0];
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fluids[index].convar[1] = fluids[ref].convar[1];
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fluids[index].convar[2] = -fluids[ref].convar[2];
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fluids[index].convar[3] = fluids[ref].convar[3];
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}
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else
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{
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fluids[index].convar[0] = fluids[ref].convar[0];
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fluids[index].convar[1] = -fluids[ref].convar[1];
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fluids[index].convar[2] = -fluids[ref].convar[2];
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fluids[index].convar[3] = fluids[ref].convar[3];
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}
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}
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}
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}
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void output_boundary_layer(Fluid2d* fluids, Block2d block, double* bcvalue, double coordx, char* label)
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{
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int order = block.ghost;
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int i;
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for (int k = 0; k < block.nx; k++)
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{
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int index = k * block.ny + order;
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if (fluids[index].coordx > coordx)
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{
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i = k;
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break;
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}
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}
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stringstream name;
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name << "result/boundarylayer_line" << label << setfill('0') << setw(5) << "step" << block.step << ".plt" << endl;
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string s;
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name >> s;
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ofstream out(s);
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out << "variables =ys,density,us,vs,pressure" << endl;
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out << "zone i = " << 1 << ",j = " << block.nodey << ", F=POINT" << endl;
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double vel = bcvalue[1];
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double nu = Mu / bcvalue[0];
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for (int j = order; j < block.ny - order; j++)
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{
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int index = i * block.ny + j;
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Convar_to_primvar_2D(fluids[index].primvar, fluids[index].convar);
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out << fluids[index].coordy / (sqrt(nu * fluids[index].coordx / vel)) << " "
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<< fluids[index].primvar[0] << " "
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<< fluids[index].primvar[1] / vel << " "
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<< fluids[index].primvar[2] / (sqrt(nu * vel / fluids[index].coordx)) << " "
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<< fluids[index].primvar[3] << " "
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<< endl;
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}
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out.close();
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}
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void output_wall_info_boundary_layer(Interface2d* xInterfaces, Interface2d* yInterfaces,
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Flux2d_gauss** xFluxes, Flux2d_gauss** yFluxes, Block2d block, double L_ref)
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{
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//there are four blocks
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int outstep = 20;
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if (block.step % outstep != 0)
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{
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return;
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}
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double t = block.t;
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double dt = block.timecoefficient[block.stages - 1][0][0] * block.dt;
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double var[8];
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Array_zero(var, 8);
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//the contribute from the bottom
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for (int i = block.ghost; i < block.ghost + block.nodex; i++)
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{
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int ref = i * (block.ny + 1) + block.ghost;
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if (yInterfaces[ref].x > 0.0)
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{
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double f_local[4];
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double derf_local[4];
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for (int m = 0; m < gausspoint; m++)
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{
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Local_to_Global(f_local, yFluxes[ref][0].gauss[m].f, yFluxes[ref][0].gauss[m].normal);
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Local_to_Global(derf_local, yFluxes[ref][0].gauss[m].derf, yFluxes[ref][0].gauss[m].normal);
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}
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double l = yInterfaces[ref].length;
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double sign = 1;
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for (int k = 0; k < 4; k++)
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{
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for (int m = 0; m < gausspoint; m++)
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{
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var[k] += sign * l * yFluxes[ref][block.stages - 1].gauss[m].x[k] / dt;
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var[k + 4] += sign * l * gauss_weight[m] * (f_local[k]) / block.dt;
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}
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}
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}
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}
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ofstream out;
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if (block.step == outstep)
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{
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out.open("result/boundary-layer-force-history.plt", ios::out);
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}
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else
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{
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out.open("result/boundary-layer-force-history.plt", ios::ate | ios::out | ios::in);
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}
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if (!out.is_open())
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{
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cout << "cannot find square-cylinder-force-history.plt" << endl;
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cout << "a new case will start" << endl;
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}
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if (block.step == outstep)
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{
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out << "# CFL number is " << block.CFL << endl;
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out << "variables = t,mass_transfer,cd,cl,heatflux,";
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out << "mass_transfer_instant, cd_instant, cl_instant, heatflux_instant" << endl;
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}
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Array_scale(var, 8, L_ref);
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out << block.t << " "
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<< var[0] << " " << var[1] << " "
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<< var[2] << " " << var[3] << " ";
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out << var[4] << " " << var[5] << " "
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<< var[6] << " " << var[7] << " ";
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out << endl;
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out.close();
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}
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void output_skin_friction_boundary_layer
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(Fluid2d* fluids, Interface2d* yInterfaces, Flux2d_gauss** yFluxes, Block2d block, double u_ref, double re_ref, double L_ref)
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{
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int outstep = 1000;
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if (block.step % outstep != 0)
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{
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return;
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}
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double t = block.t;
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double dt = block.timecoefficient[0][0][0] * block.dt;
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double var[3];
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Array_zero(var, 3);
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ofstream out;
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out.open("result/boundary-layer-skin-friction.plt", ios::out);
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out << "variables = log<sub>10</sub>Re<sub>x</sub>, log<sub>10</sub>C<sub>f</sub>, C<sub>p</sub>";
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out << endl;
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//output the data
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//the contribute from the bottom
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for (int i = block.ghost; i < block.ghost + block.nodex; i++)
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{
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int ref = i * (block.ny + 1) + block.ghost;
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int ref_cell = i * (block.ny) + block.ghost;
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if (yInterfaces[ref].x > 0.0)
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{
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Array_zero(var, 3);
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for (int k = 1; k < 3; k++)
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{
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for (int m = 0; m < gausspoint; m++)
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{
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var[k] += yFluxes[ref][0].gauss[m].x[k] / dt;
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}
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}
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var[1] = -var[1];
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var[2] = (var[2] - 1.0 / Gamma);
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double rex = yInterfaces[ref].x / L_ref * re_ref;
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for (int k = 0; k < 3; ++k)
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{
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var[k] /= (0.5 * u_ref * u_ref);
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}
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out << log10(rex) << " " << log10(var[1]) << " " << var[2] << endl;
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}
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}
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out.close();
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} |