/* This OpenCL kernel implements the Kurganov-Petrova numerical scheme for the shallow water equations, described in A. Kurganov & Guergana Petrova A Second-Order Well-Balanced Positivity Preserving Central-Upwind Scheme for the Saint-Venant System Communications in Mathematical Sciences, 5 (2007), 133-160. Copyright (C) 2016 SINTEF ICT This program is free software: you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation, either version 3 of the License, or (at your option) any later version. This program is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details. You should have received a copy of the GNU General Public License along with this program. If not, see . */ /** * Location of thread in block */ inline __device__ int get_local_id(int dim) { switch(dim) { case 0: return threadIdx.x; case 1: return threadIdx.y; case 2: return threadIdx.z; default: return -1; } } /** * Get block index */ __device__ int get_group_id(int dim) { switch(dim) { case 0: return blockIdx.x; case 1: return blockIdx.y; case 2: return blockIdx.z; default: return -1; } } /** * Location of thread in global domain */ __device__ int get_global_id(int dim) { switch(dim) { case 0: return blockDim.x*blockIdx.x + threadIdx.x; case 1: return blockDim.y*blockIdx.y + threadIdx.y; case 2: return blockDim.z*blockIdx.z + threadIdx.z; default: return -1; } } /** * Float3 operators */ inline __device__ float3 operator*(const float a, const float3 b) { return make_float3(a*b.x, a*b.y, a*b.z); } inline __device__ float3 operator/(const float3 a, const float b) { return make_float3(a.x/b, a.y/b, a.z/b); } inline __device__ float3 operator-(const float3 a, const float3 b) { return make_float3(a.x-b.x, a.y-b.y, a.z-b.z); } inline __device__ float3 operator+(const float3 a, const float3 b) { return make_float3(a.x+b.x, a.y+b.y, a.z+b.z); } inline __device__ __host__ float clamp(const float f, const float a, const float b) { return fmaxf(a, fminf(f, b)); } /** * Reads a block of data with one ghost cell for the shallow water equations */ __device__ void readBlock1(float* h_ptr_, int h_pitch_, float* hu_ptr_, int hu_pitch_, float* hv_ptr_, int hv_pitch_, float Q[3][block_height+2][block_width+2], const int nx_, const int ny_) { //Index of thread within block const int tx = get_local_id(0); const int ty = get_local_id(1); //Index of block within domain const int bx = block_width * get_group_id(0); const int by = block_height * get_group_id(1); //Read into shared memory for (int j=ty; j 0 && ti < nx_+1 && tj > 0 && tj < ny_+1) { const int i = tx + 1; //Skip local ghost cells, i.e., +1 const int j = ty + 1; float* const h_row = (float*) ((char*) h_ptr_ + h_pitch_*tj); float* const hu_row = (float*) ((char*) hu_ptr_ + hu_pitch_*tj); float* const hv_row = (float*) ((char*) hv_ptr_ + hv_pitch_*tj); h_row[ti] = Q[0][j][i]; hu_row[ti] = Q[1][j][i]; hv_row[ti] = Q[2][j][i]; } } /** * Writes a block of data to global memory for the shallow water equations. */ __device__ void writeBlock2(float* h_ptr_, int h_pitch_, float* hu_ptr_, int hu_pitch_, float* hv_ptr_, int hv_pitch_, float Q[3][block_height+4][block_width+4], const int nx_, const int ny_) { //Index of thread within block const int tx = get_local_id(0); const int ty = get_local_id(1); //Index of cell within domain const int ti = get_global_id(0) + 2; //Skip global ghost cells, i.e., +2 const int tj = get_global_id(1) + 2; //Only write internal cells if (ti > 1 && ti < nx_+2 && tj > 1 && tj < ny_+2) { const int i = tx + 2; //Skip local ghost cells, i.e., +2 const int j = ty + 2; float* const h_row = (float*) ((char*) h_ptr_ + h_pitch_*tj); float* const hu_row = (float*) ((char*) hu_ptr_ + hu_pitch_*tj); float* const hv_row = (float*) ((char*) hv_ptr_ + hv_pitch_*tj); h_row[ti] = Q[0][j][i]; hu_row[ti] = Q[1][j][i]; hv_row[ti] = Q[2][j][i]; } } /** * No flow boundary conditions for the shallow water equations * with one ghost cell in each direction */ __device__ void noFlowBoundary1(float Q[3][block_height+2][block_width+2], const int nx_, const int ny_) { //Global index const int ti = get_global_id(0) + 1; //Skip global ghost cells, i.e., +1 const int tj = get_global_id(1) + 1; //Block-local indices const int tx = get_local_id(0); const int ty = get_local_id(1); const int i = tx + 1; //Skip local ghost cells, i.e., +1 const int j = ty + 1; //Fix boundary conditions if (ti == 1) { Q[0][j][i-1] = Q[0][j][i]; Q[1][j][i-1] = -Q[1][j][i]; Q[2][j][i-1] = Q[2][j][i]; } if (ti == nx_) { Q[0][j][i+1] = Q[0][j][i]; Q[1][j][i+1] = -Q[1][j][i]; Q[2][j][i+1] = Q[2][j][i]; } if (tj == 1) { Q[0][j-1][i] = Q[0][j][i]; Q[1][j-1][i] = Q[1][j][i]; Q[2][j-1][i] = -Q[2][j][i]; } if (tj == ny_) { Q[0][j+1][i] = Q[0][j][i]; Q[1][j+1][i] = Q[1][j][i]; Q[2][j+1][i] = -Q[2][j][i]; } } /** * No flow boundary conditions for the shallow water equations * with two ghost cells in each direction */ __device__ void noFlowBoundary2(float Q[3][block_height+4][block_width+4], const int nx_, const int ny_) { //Global index const int ti = get_global_id(0) + 2; //Skip global ghost cells, i.e., +2 const int tj = get_global_id(1) + 2; //Block-local indices const int tx = get_local_id(0); const int ty = get_local_id(1); const int i = tx + 2; //Skip local ghost cells, i.e., +2 const int j = ty + 2; if (ti == 2) { Q[0][j][i-1] = Q[0][j][i]; Q[1][j][i-1] = -Q[1][j][i]; Q[2][j][i-1] = Q[2][j][i]; Q[0][j][i-2] = Q[0][j][i+1]; Q[1][j][i-2] = -Q[1][j][i+1]; Q[2][j][i-2] = Q[2][j][i+1]; } if (ti == nx_+1) { Q[0][j][i+1] = Q[0][j][i]; Q[1][j][i+1] = -Q[1][j][i]; Q[2][j][i+1] = Q[2][j][i]; Q[0][j][i+2] = Q[0][j][i-1]; Q[1][j][i+2] = -Q[1][j][i-1]; Q[2][j][i+2] = Q[2][j][i-1]; } if (tj == 2) { Q[0][j-1][i] = Q[0][j][i]; Q[1][j-1][i] = Q[1][j][i]; Q[2][j-1][i] = -Q[2][j][i]; Q[0][j-2][i] = Q[0][j+1][i]; Q[1][j-2][i] = Q[1][j+1][i]; Q[2][j-2][i] = -Q[2][j+1][i]; } if (tj == ny_+1) { Q[0][j+1][i] = Q[0][j][i]; Q[1][j+1][i] = Q[1][j][i]; Q[2][j+1][i] = -Q[2][j][i]; Q[0][j+2][i] = Q[0][j-1][i]; Q[1][j+2][i] = Q[1][j-1][i]; Q[2][j+2][i] = -Q[2][j-1][i]; } } /** * Evolves the solution in time along the x axis (dimensional splitting) */ __device__ void evolveF1(float Q[3][block_height+2][block_width+2], float F[3][block_height+1][block_width+1], const int nx_, const int ny_, const float dx_, const float dt_) { //Index of thread within block const int tx = get_local_id(0); const int ty = get_local_id(1); //Index of cell within domain const int ti = get_global_id(0) + 1; //Skip global ghost cells, i.e., +1 const int tj = get_global_id(1) + 1; if (ti > 0 && ti < nx_+1 && tj > 0 && tj < ny_+1) { const int i = tx + 1; //Skip local ghost cells, i.e., +1 const int j = ty + 1; Q[0][j][i] = Q[0][j][i] + (F[0][ty][tx] - F[0][ty][tx+1]) * dt_ / dx_; Q[1][j][i] = Q[1][j][i] + (F[1][ty][tx] - F[1][ty][tx+1]) * dt_ / dx_; Q[2][j][i] = Q[2][j][i] + (F[2][ty][tx] - F[2][ty][tx+1]) * dt_ / dx_; } } /** * Evolves the solution in time along the x axis (dimensional splitting) */ __device__ void evolveF2(float Q[3][block_height+4][block_width+4], float F[3][block_height+1][block_width+1], const int nx_, const int ny_, const float dx_, const float dt_) { //Index of thread within block const int tx = get_local_id(0); const int ty = get_local_id(1); //Index of cell within domain const int ti = get_global_id(0) + 2; //Skip global ghost cells, i.e., +2 const int tj = get_global_id(1) + 2; if (ti > 1 && ti < nx_+2 && tj > 1 && tj < ny_+2) { const int i = tx + 2; //Skip local ghost cells, i.e., +1 const int j = ty + 2; Q[0][j][i] = Q[0][j][i] + (F[0][ty][tx] - F[0][ty][tx+1]) * dt_ / dx_; Q[1][j][i] = Q[1][j][i] + (F[1][ty][tx] - F[1][ty][tx+1]) * dt_ / dx_; Q[2][j][i] = Q[2][j][i] + (F[2][ty][tx] - F[2][ty][tx+1]) * dt_ / dx_; } } /** * Evolves the solution in time along the y axis (dimensional splitting) */ __device__ void evolveG1(float Q[3][block_height+2][block_width+2], float G[3][block_height+1][block_width+1], const int nx_, const int ny_, const float dy_, const float dt_) { //Index of thread within block const int tx = get_local_id(0); const int ty = get_local_id(1); //Index of cell within domain const int ti = get_global_id(0) + 1; //Skip global ghost cells, i.e., +1 const int tj = get_global_id(1) + 1; if (ti > 0 && ti < nx_+1 && tj > 0 && tj < ny_+1) { const int i = tx + 1; //Skip local ghost cells, i.e., +1 const int j = ty + 1; Q[0][j][i] = Q[0][j][i] + (G[0][ty][tx] - G[0][ty+1][tx]) * dt_ / dy_; Q[1][j][i] = Q[1][j][i] + (G[1][ty][tx] - G[1][ty+1][tx]) * dt_ / dy_; Q[2][j][i] = Q[2][j][i] + (G[2][ty][tx] - G[2][ty+1][tx]) * dt_ / dy_; } } /** * Evolves the solution in time along the y axis (dimensional splitting) */ __device__ void evolveG2(float Q[3][block_height+4][block_width+4], float G[3][block_height+1][block_width+1], const int nx_, const int ny_, const float dy_, const float dt_) { //Index of thread within block const int tx = get_local_id(0); const int ty = get_local_id(1); //Index of cell within domain const int ti = get_global_id(0) + 2; //Skip global ghost cells, i.e., +2 const int tj = get_global_id(1) + 2; if (ti > 1 && ti < nx_+2 && tj > 1 && tj < ny_+2) { const int i = tx + 2; //Skip local ghost cells, i.e., +2 const int j = ty + 2; Q[0][j][i] = Q[0][j][i] + (G[0][ty][tx] - G[0][ty+1][tx]) * dt_ / dy_; Q[1][j][i] = Q[1][j][i] + (G[1][ty][tx] - G[1][ty+1][tx]) * dt_ / dy_; Q[2][j][i] = Q[2][j][i] + (G[2][ty][tx] - G[2][ty+1][tx]) * dt_ / dy_; } } /** * Reconstructs a slope using the minmod limiter based on three * consecutive values */ __device__ float minmodSlope(float left, float center, float right, float theta) { const float backward = (center - left) * theta; const float central = (right - left) * 0.5f; const float forward = (right - center) * theta; return 0.25f *copysign(1.0f, backward) *(copysign(1.0f, backward) + copysign(1.0f, central)) *(copysign(1.0f, central) + copysign(1.0f, forward)) *min( min(fabs(backward), fabs(central)), fabs(forward) ); } /** * Reconstructs a minmod slope for a whole block along x */ __device__ void minmodSlopeX(float Q[3][block_height+4][block_width+4], float Qx[3][block_height+2][block_width+2], const float theta_) { //Index of thread within block const int tx = get_local_id(0); const int ty = get_local_id(1); //Reconstruct slopes along x axis { const int j = ty; const int l = j + 2; //Skip ghost cells for (int i=tx; i h_l) ? q_l_tmp : 1.0f; const float q_r = (h_dag > h_r) ? q_r_tmp : 1.0f; // Compute wave speed estimates const float S_l = u_l - c_l*q_l; const float S_r = u_r + c_r*q_r; //Upwind selection if (S_l >= 0.0f) { return F_func(Q_l, g_); } else if (S_r <= 0.0f) { return F_func(Q_r, g_); } //Or estimate flux in the star region else { const float3 F_l = F_func(Q_l, g_); const float3 F_r = F_func(Q_r, g_); const float3 flux = (S_r*F_l - S_l*F_r + S_r*S_l*(Q_r - Q_l)) / (S_r-S_l); return flux; } } /** * Harten-Lax-van Leer with contact discontinuity (Toro 2001, p 181) */ __device__ float3 HLLC_flux(const float3 Q_l, const float3 Q_r, const float g_) { const float h_l = Q_l.x; const float h_r = Q_r.x; // Calculate velocities const float u_l = Q_l.y / h_l; const float u_r = Q_r.y / h_r; // Estimate the potential wave speeds const float c_l = sqrt(g_*h_l); const float c_r = sqrt(g_*h_r); // Compute h in the "star region", h^dagger const float h_dag = 0.5f * (h_l+h_r) - 0.25f * (u_r-u_l)*(h_l+h_r)/(c_l+c_r); const float q_l_tmp = sqrt(0.5f * ( (h_dag+h_l)*h_dag / (h_l*h_l) ) ); const float q_r_tmp = sqrt(0.5f * ( (h_dag+h_r)*h_dag / (h_r*h_r) ) ); const float q_l = (h_dag > h_l) ? q_l_tmp : 1.0f; const float q_r = (h_dag > h_r) ? q_r_tmp : 1.0f; // Compute wave speed estimates const float S_l = u_l - c_l*q_l; const float S_r = u_r + c_r*q_r; const float S_star = ( S_l*h_r*(u_r - S_r) - S_r*h_l*(u_l - S_l) ) / ( h_r*(u_r - S_r) - h_l*(u_l - S_l) ); const float3 F_l = F_func(Q_l, g_); const float3 F_r = F_func(Q_r, g_); //Upwind selection if (S_l >= 0.0f) { return F_l; } else if (S_r <= 0.0f) { return F_r; } //Or estimate flux in the "left star" region else if (S_l <= 0.0f && 0.0f <=S_star) { const float v_l = Q_l.z / h_l; const float3 Q_star_l = h_l * (S_l - u_l) / (S_l - S_star) * make_float3(1, S_star, v_l); const float3 flux = F_l + S_l*(Q_star_l - Q_l); return flux; } //Or estimate flux in the "righ star" region else if (S_star <= 0.0f && 0.0f <=S_r) { const float v_r = Q_r.z / h_r; const float3 Q_star_r = h_r * (S_r - u_r) / (S_r - S_star) * make_float3(1, S_star, v_r); const float3 flux = F_r + S_r*(Q_star_r - Q_r); return flux; } else { return make_float3(-99999.9f, -99999.9f, -99999.9f); //Something wrong here } } /** * Superbee flux limiter for WAF. * Related to superbee limiter so that WAF_superbee(r, c) = 1 - (1-|c|)*superbee(r) * @param r_ the ratio of upwind change (see Toro 2001, p. 203/204) * @param c_ the courant number for wave k, dt*S_k/dx */ __device__ float WAF_superbee(float r_, float c_) { // r <= 0.0 if (r_ <= 0.0f) { return 1.0f; } // 0.0 <= r <= 1/2 else if (r_ <= 0.5f) { return 1.0f - 2.0f*(1.0f - fabsf(c_))*r_; } // 1/2 <= r <= 1 else if (r_ <= 1.0f) { return fabs(c_); } // 1 <= r <= 2 else if (r_ <= 2.0f) { return 1.0f - (1.0f - fabsf(c_))*r_; } // r >= 2 else { return 2.0f*fabsf(c_) - 1.0f; } } __device__ float WAF_albada(float r_, float c_) { if (r_ <= 0.0f) { return 1.0f; } else { return 1.0f - (1.0f - fabsf(c_)) * r_ * (1.0f + r_) / (1.0f + r_*r_); } } __device__ float WAF_minbee(float r_, float c_) { r_ = fmaxf(-1.0f, fminf(2.0f, r_)); if (r_ <= 0.0f) { return 1.0f; } if (r_ >= 0.0f && r_ <= 1.0f) { return 1.0f - (1.0f - fabsf(c_)) * r_; } else { return fabsf(c_); } } __device__ float WAF_minmod(float r_, float c_) { return 1.0f - (1.0f - fabsf(c_)) * fmaxf(0.0f, fminf(1.0f, r_)); } __device__ float minmod(float r_) { return fmaxf(0.0f, fminf(1.0f, r_)); } __device__ float generalized_minmod(float r_, float theta_) { return fmaxf(0.0f, fminf(theta_*r_, fminf( (1.0f + r_) / 2.0f, theta_))); } __device__ float superbee(float r_) { return fmaxf(0.0f, fmaxf(fminf(2.0f*r_, 1.0f), fminf(r_, 2.0f))); } __device__ float vanAlbada1(float r_) { return (r_*r_ + r_) / (r_*r_ + 1.0f); } __device__ float vanLeer(float r_) { return (r_ + fabsf(r_)) / (1.0f + fabsf(r_)); } __device__ float limiterToWAFLimiter(float r_, float c_) { return 1.0f - (1.0f - fabsf(c_))*r_; } __device__ float desingularize(float x_, float eps_) { return copysign(1.0f, x_)*fmaxf(fabsf(x_), fminf(x_*x_/(2.0f*eps_)+0.5f*eps_, eps_)); } // Compute h in the "star region", h^dagger __device__ float computeHStar(float h_l, float h_r, float u_l, float u_r, float c_l, float c_r, float g_) { //return 0.5f * (h_l+h_r) - 0.25f * (u_r-u_l)*(h_l+h_r)/(c_l+c_r); const float h_tmp = 0.5f * (c_l + c_r) + 0.25f * (u_l - u_r); return h_tmp*h_tmp / g_; } /** * Weighted average flux (Toro 2001, p 200) for interface {i+1/2} * @param r_ The flux limiter parameter (see Toro 2001, p. 203) * @param Q_l2 Q_{i-1} * @param Q_l1 Q_{i} * @param Q_r1 Q_{i+1} * @param Q_r2 Q_{i+2} */ __device__ float3 WAF_1D_flux(const float3 Q_l2, const float3 Q_l1, const float3 Q_r1, const float3 Q_r2, const float g_, const float dx_, const float dt_) { const float h_l = Q_l1.x; const float h_r = Q_r1.x; const float h_l2 = Q_l2.x; const float h_r2 = Q_r2.x; // Calculate velocities const float u_l = Q_l1.y / h_l; const float u_r = Q_r1.y / h_r; const float u_l2 = Q_l2.y / h_l2; const float u_r2 = Q_r2.y / h_r2; const float v_l = Q_l1.z / h_l; const float v_r = Q_r1.z / h_r; const float v_l2 = Q_l2.z / h_l2; const float v_r2 = Q_r2.z / h_r2; // Estimate the potential wave speeds const float c_l = sqrt(g_*h_l); const float c_r = sqrt(g_*h_r); const float c_l2 = sqrt(g_*h_l2); const float c_r2 = sqrt(g_*h_r2); // Compute h in the "star region", h^dagger const float h_dag_l = computeHStar(h_l2, h_l, u_l2, u_l, c_l2, c_l, g_); const float h_dag = computeHStar( h_l, h_r, u_l, u_r, c_l, c_r, g_); const float h_dag_r = computeHStar( h_r, h_r2, u_r, u_r2, c_r, c_r2, g_); const float q_l_tmp = sqrt(0.5f * ( (h_dag+h_l)*h_dag ) ) / h_l; const float q_r_tmp = sqrt(0.5f * ( (h_dag+h_r)*h_dag ) ) / h_r; const float q_l = (h_dag > h_l) ? q_l_tmp : 1.0f; const float q_r = (h_dag > h_r) ? q_r_tmp : 1.0f; // Compute wave speed estimates const float S_l = u_l - c_l*q_l; const float S_r = u_r + c_r*q_r; const float S_star = ( S_l*h_r*(u_r - S_r) - S_r*h_l*(u_l - S_l) ) / ( h_r*(u_r - S_r) - h_l*(u_l - S_l) ); const float3 Q_star_l = h_l * (S_l - u_l) / (S_l - S_star) * make_float3(1.0, S_star, v_l); const float3 Q_star_r = h_r * (S_r - u_r) / (S_r - S_star) * make_float3(1.0, S_star, v_r); // Estimate the fluxes in the four regions const float3 F_1 = F_func(Q_l1, g_); const float3 F_4 = F_func(Q_r1, g_); const float3 F_2 = F_1 + S_l*(Q_star_l - Q_l1); const float3 F_3 = F_4 + S_r*(Q_star_r - Q_r1); //const float3 F_2 = F_func(Q_star_l, g_); //const float3 F_3 = F_func(Q_star_r, g_); // Compute the courant numbers for the waves const float c_1 = S_l * dt_ / dx_; const float c_2 = S_star * dt_ / dx_; const float c_3 = S_r * dt_ / dx_; // Compute the "upwind change" vectors for the i-3/2 and i+3/2 interfaces const float eps = 1.0e-6f; const float r_1 = desingularize( (c_1 > 0.0f) ? (h_dag_l - h_l2) : (h_dag_r - h_r), eps) / desingularize((h_dag - h_l), eps); const float r_2 = desingularize( (c_2 > 0.0f) ? (v_l - v_l2) : (v_r2 - v_r), eps ) / desingularize((v_r - v_l), eps); const float r_3 = desingularize( (c_3 > 0.0f) ? (h_l - h_dag_l) : (h_r2 - h_dag_r), eps ) / desingularize((h_r - h_dag), eps); /* const float eps1 = 1.0e-6f; const float eps2 = eps1;//*1.0e-1f; const float rh_m = desingularize((h_l - h_l2), eps1) / desingularize((h_r - h_l), eps2); const float rh_p = desingularize((h_r2 - h_r), eps1) / desingularize((h_r - h_l), eps2); const float rv_m = desingularize((v_l - v_l2), eps1) / desingularize((v_r - v_l), eps2); const float rv_p = desingularize((v_r2 - v_r), eps1) / desingularize((v_r - v_l), eps2); // Compute the r parameters for the flux limiter const float rh_1 = (c_1 > 0.0f) ? rh_m : rh_p; const float rv_1 = (c_1 > 0.0f) ? rv_m : rv_p; const float rh_2 = (c_2 > 0.0f) ? rh_m : rh_p; const float rv_2 = (c_2 > 0.0f) ? rv_m : rv_p; const float rh_3 = (c_3 > 0.0f) ? rh_m : rh_p; const float rv_3 = (c_3 > 0.0f) ? rv_m : rv_p; const float r_1 = rh_1; const float r_2 = rv_2; const float r_3 = rh_3; */ // Compute the limiter // We use h for the nonlinear waves, and v for the middle shear wave const float A_1 = copysign(1.0f, c_1) * limiterToWAFLimiter(generalized_minmod(r_1, 1.9f), c_1); const float A_2 = copysign(1.0f, c_2) * limiterToWAFLimiter(generalized_minmod(r_2, 1.9f), c_2); //Middle shear wave const float A_3 = copysign(1.0f, c_3) * limiterToWAFLimiter(generalized_minmod(r_3, 1.9f), c_3); //Average the fluxes const float3 flux = 0.5f*( F_1 + F_4 ) - 0.5f*( A_1 * (F_2 - F_1) + A_2 * (F_3 - F_2) + A_3 * (F_4 - F_3) ); return flux; } /** * Lax-Friedrichs flux (Toro 2001, p 163) */ __device__ float3 LxF_1D_flux(const float3 Q_l, const float3 Q_r, const float g_, const float dx_, const float dt_) { const float3 F_l = F_func(Q_l, g_); const float3 F_r = F_func(Q_r, g_); return 0.5f*(F_l + F_r) + (dx_/(2.0f*dt_))*(Q_l - Q_r); } /** * Lax-Friedrichs extended to 2D */ __device__ float3 LxF_2D_flux(const float3 Q_l, const float3 Q_r, const float g_, const float dx_, const float dt_) { const float3 F_l = F_func(Q_l, g_); const float3 F_r = F_func(Q_r, g_); //Note numerical diffusion for 2D here (0.25) return 0.5f*(F_l + F_r) + (dx_/(4.0f*dt_))*(Q_l - Q_r); } /** * Richtmeyer / Two-step Lax-Wendroff flux (Toro 2001, p 164) */ __device__ float3 LxW2_1D_flux(const float3 Q_l, const float3 Q_r, const float g_, const float dx_, const float dt_) { const float3 F_l = F_func(Q_l, g_); const float3 F_r = F_func(Q_r, g_); const float3 Q_lw2 = 0.5f*(Q_l + Q_r) + (dt_/(2.0f*dx_))*(F_l - F_r); return F_func(Q_lw2, g_); } /** * Godunovs centered scheme (Toro 2001, p 165) */ __device__ float3 GodC_1D_flux(const float3 Q_l, const float3 Q_r, const float g_, const float dx_, const float dt_) { const float3 F_l = F_func(Q_l, g_); const float3 F_r = F_func(Q_r, g_); const float3 Q_godc = 0.5f*(Q_l + Q_r) + (dt_/dx_)*(F_l - F_r); return F_func(Q_godc, g_); } /** * First Ordered Centered (Toro 2001, p.163) */ __device__ float3 FORCE_1D_flux(const float3 Q_l, const float3 Q_r, const float g_, const float dx_, const float dt_) { const float3 F_lf = LxF_1D_flux(Q_l, Q_r, g_, dx_, dt_); const float3 F_lw2 = LxW2_1D_flux(Q_l, Q_r, g_, dx_, dt_); return 0.5f*(F_lf + F_lw2); }