xref: /libCEED/examples/fluids/qfunctions/riemann_solver.h (revision 17937fbf32b4e8f1ab6f0d029b0dedadbd90d996) !
1 // Copyright (c) 2017-2022, Lawrence Livermore National Security, LLC and other CEED contributors.
2 // All Rights Reserved. See the top-level LICENSE and NOTICE files for details.
3 //
4 // SPDX-License-Identifier: BSD-2-Clause
5 //
6 // This file is part of CEED:  http://github.com/ceed
7 
8 /// @file
9 /// Helper functions for solving the Riemann problem.
10 // The left and right states are specified from the perspective of an outward-facing normal vector pointing left to right:
11 //
12 //     (domain)
13 //    /               (outward facing normal)
14 // |------------|   /
15 // |            |  /
16 // |    Left    |---->  Right
17 // | (Interior) |    (Exterior)
18 // |------------|
19 //
20 // The right state is exterior to the domain and the left state is the interior to the domain.
21 // Much of the work references Eleuterio F. Toro's "Riemann Solvers and Numerical Methods for Fluid Dynamics", 2009
22 
23 #ifndef riemann_solver_h
24 #define riemann_solver_h
25 
26 #include "newtonian_state.h"
27 #include "newtonian_types.h"
28 
29 enum RiemannFluxType_ { RIEMANN_HLL, RIEMANN_HLLC };
30 typedef enum RiemannFluxType_ RiemannFluxType;
31 
32 typedef struct {
33   CeedScalar left, right;
34 } RoeWeights;
35 
36 CEED_QFUNCTION_HELPER RoeWeights RoeSetup(CeedScalar rho_left, CeedScalar rho_right) {
37   CeedScalar sqrt_left = sqrt(rho_left), sqrt_right = sqrt(rho_right);
38   RoeWeights w = {sqrt_left / (sqrt_left + sqrt_right), sqrt_right / (sqrt_left + sqrt_right)};
39   return w;
40 }
41 
42 CEED_QFUNCTION_HELPER RoeWeights RoeSetup_fwd(CeedScalar rho_left, CeedScalar rho_right, CeedScalar drho_left, CeedScalar drho_right) {
43   CeedScalar sqrt_left = sqrt(rho_left), sqrt_right = sqrt(rho_right);
44   CeedScalar square_sum_root = Square(sqrt_left + sqrt_right);
45   CeedScalar r_right = (sqrt_left / (2 * sqrt_right * square_sum_root)) * drho_right - (sqrt_right / (2 * sqrt_left * square_sum_root)) * drho_left;
46   CeedScalar r_left  = (sqrt_right / (2 * sqrt_left * square_sum_root)) * drho_left - (sqrt_left / (2 * sqrt_right * square_sum_root)) * drho_right;
47   RoeWeights dw      = {r_left, r_right};
48   return dw;
49 }
50 
51 CEED_QFUNCTION_HELPER CeedScalar RoeAverage(RoeWeights r, CeedScalar q_left, CeedScalar q_right) { return r.left * q_left + r.right * q_right; }
52 
53 CEED_QFUNCTION_HELPER CeedScalar RoeAverage_fwd(RoeWeights r, RoeWeights dr, CeedScalar q_left, CeedScalar q_right, CeedScalar dq_left,
54                                                 CeedScalar dq_right) {
55   return q_right * dr.right + q_left * dr.left + r.right * dq_right + r.left * dq_left;
56 }
57 
58 CEED_QFUNCTION_HELPER StateConservative Flux_HLL(State left, State right, StateConservative flux_left, StateConservative flux_right,
59                                                  CeedScalar s_left, CeedScalar s_right) {
60   CeedScalar U_left[5], U_right[5], F_right[5], F_left[5], F_hll[5];
61   UnpackState_U(left.U, U_left);
62   UnpackState_U(right.U, U_right);
63   UnpackState_U(flux_left, F_left);
64   UnpackState_U(flux_right, F_right);
65   for (int i = 0; i < 5; i++) {
66     F_hll[i] = (s_right * F_left[i] - s_left * F_right[i] + s_left * s_right * (U_right[i] - U_left[i])) / (s_right - s_left);
67   }
68   StateConservative F = {
69       F_hll[0],
70       {F_hll[1], F_hll[2], F_hll[3]},
71       F_hll[4],
72   };
73   return F;
74 }
75 
76 CEED_QFUNCTION_HELPER StateConservative Flux_HLL_fwd(State left, State right, State dleft, State dright, StateConservative flux_left,
77                                                      StateConservative flux_right, StateConservative dflux_left, StateConservative dflux_right,
78                                                      CeedScalar S_l, CeedScalar S_r, CeedScalar dS_l, CeedScalar dS_r) {
79   CeedScalar U_l[5], U_r[5], F_r[5], F_l[5];
80   UnpackState_U(left.U, U_l);
81   UnpackState_U(right.U, U_r);
82   UnpackState_U(flux_left, F_l);
83   UnpackState_U(flux_right, F_r);
84 
85   CeedScalar dU_l[5], dU_r[5], dF_r[5], dF_l[5], dF_hll[5] = {0.};
86   UnpackState_U(dleft.U, dU_l);
87   UnpackState_U(dright.U, dU_r);
88   UnpackState_U(dflux_left, dF_l);
89   UnpackState_U(dflux_right, dF_r);
90   for (int i = 0; i < 5; i++) {
91     const CeedScalar U_diff      = U_r[i] - U_l[i];
92     const CeedScalar S_diff      = S_r - S_l;
93     const CeedScalar F_hll_denom = S_r * F_l[i] - S_l * F_r[i] + S_l * S_r * U_diff;
94 
95     dF_hll[i] += ((F_l[i] + S_r * U_diff) * S_diff - F_hll_denom) / Square(S_diff) * dS_r;
96     dF_hll[i] += ((-F_r[i] + S_r * U_diff) * S_diff + F_hll_denom) / Square(S_diff) * dS_l;
97     dF_hll[i] += (S_r * dF_l[i] - S_l * dF_r[i] + S_r * S_l * dU_r[i] - S_r * S_l * dU_l[i]) / S_diff;
98   }
99   StateConservative dF = {
100       dF_hll[0],
101       {dF_hll[1], dF_hll[2], dF_hll[3]},
102       dF_hll[4],
103   };
104   return dF;
105 }
106 
107 CEED_QFUNCTION_HELPER void ComputeHLLSpeeds_Roe(NewtonianIdealGasContext gas, State left, CeedScalar u_left, State right, CeedScalar u_right,
108                                                 CeedScalar *s_left, CeedScalar *s_right) {
109   const CeedScalar gamma = HeatCapacityRatio(gas);
110 
111   RoeWeights r = RoeSetup(left.U.density, right.U.density);
112   // Speed estimate
113   // Roe average eigenvalues for left and right non-linear waves.
114   // Stability requires that these speed estimates are *at least* as fast as the physical wave speeds.
115   CeedScalar u_roe = RoeAverage(r, u_left, u_right);
116 
117   // TODO: revisit this for gravity
118   CeedScalar H_left  = TotalSpecificEnthalpy(gas, left);
119   CeedScalar H_right = TotalSpecificEnthalpy(gas, right);
120   CeedScalar H_roe   = RoeAverage(r, H_left, H_right);
121   CeedScalar a_roe   = sqrt((gamma - 1) * (H_roe - 0.5 * Square(u_roe)));
122 
123   // Einfeldt (1988) justifies (and Toro's book repeats) that Roe speeds can be used here.
124   *s_left  = u_roe - a_roe;
125   *s_right = u_roe + a_roe;
126 }
127 
128 CEED_QFUNCTION_HELPER void ComputeHLLSpeeds_Roe_fwd(NewtonianIdealGasContext gas, State left, State dleft, CeedScalar u_left, CeedScalar du_left,
129                                                     State right, State dright, CeedScalar u_right, CeedScalar du_right, CeedScalar *s_left,
130                                                     CeedScalar *ds_left, CeedScalar *s_right, CeedScalar *ds_right) {
131   const CeedScalar gamma = HeatCapacityRatio(gas);
132 
133   RoeWeights r  = RoeSetup(left.U.density, right.U.density);
134   RoeWeights dr = RoeSetup_fwd(left.U.density, right.U.density, dleft.U.density, dright.U.density);
135   // Speed estimate
136   // Roe average eigenvalues for left and right non-linear waves.
137   // Stability requires that these speed estimates are *at least* as fast as the physical wave speeds.
138   CeedScalar u_roe  = RoeAverage(r, u_left, u_right);
139   CeedScalar du_roe = RoeAverage_fwd(r, dr, u_left, u_right, du_left, du_right);
140 
141   CeedScalar H_left   = TotalSpecificEnthalpy(gas, left);
142   CeedScalar H_right  = TotalSpecificEnthalpy(gas, right);
143   CeedScalar dH_left  = TotalSpecificEnthalpy_fwd(gas, left, dleft);
144   CeedScalar dH_right = TotalSpecificEnthalpy_fwd(gas, right, dright);
145 
146   CeedScalar H_roe  = RoeAverage(r, H_left, H_right);
147   CeedScalar dH_roe = RoeAverage_fwd(r, dr, H_left, H_right, dH_left, dH_right);
148   CeedScalar a_roe  = sqrt((gamma - 1) * (H_roe - 0.5 * Square(u_roe)));
149   CeedScalar da_roe = 0.5 * (gamma - 1) / sqrt(H_roe) * dH_roe - 0.5 * sqrt(gamma - 1) * u_roe / sqrt(H_roe - 0.5 * Square(u_roe)) * du_roe;
150 
151   *s_left   = u_roe - a_roe;
152   *ds_left  = du_roe - da_roe;
153   *s_right  = u_roe + a_roe;
154   *ds_right = du_roe + da_roe;
155 }
156 
157 // *****************************************************************************
158 // @brief Harten Lax VanLeer (HLL) approximate Riemann solver.
159 // Taking in two states (left, right) and returns RiemannFlux_HLL.
160 // The left and right states are specified from the perspective of an outward-facing normal vector pointing left to right.
161 //
162 // @param[in] gas    NewtonianIdealGasContext for the fluid
163 // @param[in] left   Fluid state of the domain interior (the current solution)
164 // @param[in] right  Fluid state of the domain exterior (free stream conditions)
165 // @param[in] normal Normalized, outward facing boundary normal vector
166 //
167 // @return StateConservative with HLL Riemann Flux
168 // *****************************************************************************
169 CEED_QFUNCTION_HELPER StateConservative RiemannFlux_HLL(NewtonianIdealGasContext gas, State left, State right, const CeedScalar normal[3]) {
170   StateConservative flux_left  = FluxInviscidDotNormal(gas, left, normal);
171   StateConservative flux_right = FluxInviscidDotNormal(gas, right, normal);
172 
173   CeedScalar u_left  = Dot3(left.Y.velocity, normal);
174   CeedScalar u_right = Dot3(right.Y.velocity, normal);
175 
176   CeedScalar s_left, s_right;
177   ComputeHLLSpeeds_Roe(gas, left, u_left, right, u_right, &s_left, &s_right);
178 
179   // Compute HLL flux
180   if (0 <= s_left) {
181     return flux_left;
182   } else if (s_right <= 0) {
183     return flux_right;
184   } else {
185     return Flux_HLL(left, right, flux_left, flux_right, s_left, s_right);
186   }
187 }
188 
189 // *****************************************************************************
190 // @brief Forward-mode Derivative of Harten Lax VanLeer (HLL) approximate Riemann solver.
191 //
192 // @param gas    NewtonianIdealGasContext for the fluid
193 // @param left   Fluid state of the domain interior (the current solution)
194 // @param right  Fluid state of the domain exterior (free stream conditions)
195 // @param dleft  Derivative of fluid state of the domain interior (the current solution)
196 // @param dright Derivative of fluid state of the domain exterior (free stream conditions)
197 // @param normal Normalized, outward facing boundary normal vector
198 //
199 // @return StateConservative with derivative of HLL Riemann Flux
200 // *****************************************************************************
201 CEED_QFUNCTION_HELPER StateConservative RiemannFlux_HLL_fwd(NewtonianIdealGasContext gas, State left, State dleft, State right, State dright,
202                                                             const CeedScalar normal[3]) {
203   StateConservative flux_left   = FluxInviscidDotNormal(gas, left, normal);
204   StateConservative flux_right  = FluxInviscidDotNormal(gas, right, normal);
205   StateConservative dflux_left  = FluxInviscidDotNormal_fwd(gas, left, dleft, normal);
206   StateConservative dflux_right = FluxInviscidDotNormal_fwd(gas, right, dright, normal);
207 
208   CeedScalar u_left   = Dot3(left.Y.velocity, normal);
209   CeedScalar u_right  = Dot3(right.Y.velocity, normal);
210   CeedScalar du_left  = Dot3(dleft.Y.velocity, normal);
211   CeedScalar du_right = Dot3(dright.Y.velocity, normal);
212 
213   CeedScalar s_left, ds_left, s_right, ds_right;
214   ComputeHLLSpeeds_Roe_fwd(gas, left, dleft, u_left, du_left, right, dright, u_right, du_right, &s_left, &ds_left, &s_right, &ds_right);
215 
216   if (0 <= s_left) {
217     return dflux_left;
218   } else if (s_right <= 0) {
219     return dflux_right;
220   } else {
221     return Flux_HLL_fwd(left, right, dleft, dright, flux_left, flux_right, dflux_left, dflux_right, s_left, s_right, ds_left, ds_right);
222   }
223 }
224 
225 CEED_QFUNCTION_HELPER StateConservative RiemannFlux_HLLC_Star(NewtonianIdealGasContext gas, State side, StateConservative F_side,
226                                                               const CeedScalar normal[3], CeedScalar u_side, CeedScalar s_side, CeedScalar s_star) {
227   CeedScalar fact  = side.U.density * (s_side - u_side) / (s_side - s_star);
228   CeedScalar denom = side.U.density * (s_side - u_side);
229   // U_* = fact * star
230   StateConservative star = {
231       1.0,
232       {
233         side.Y.velocity[0] + (s_star - u_side) * normal[0],
234         side.Y.velocity[1] + (s_star - u_side) * normal[1],
235         side.Y.velocity[2] + (s_star - u_side) * normal[2],
236         },
237       side.U.E_total / side.U.density  //
238           + (s_star - u_side) * (s_star + side.Y.pressure / denom)
239   };
240   return StateConservativeAXPBYPCZ(1, F_side, s_side * fact, star, -s_side, side.U);
241 }
242 
243 CEED_QFUNCTION_HELPER StateConservative RiemannFlux_HLLC_Star_fwd(NewtonianIdealGasContext gas, State side, State dside, StateConservative F_side,
244                                                                   StateConservative dF_side, const CeedScalar normal[3], CeedScalar u_side,
245                                                                   CeedScalar du_side, CeedScalar s_side, CeedScalar ds_side, CeedScalar s_star,
246                                                                   CeedScalar ds_star) {
247   CeedScalar fact  = side.U.density * (s_side - u_side) / (s_side - s_star);
248   CeedScalar dfact = (side.U.density * (ds_side - du_side) + dside.U.density * (s_side - u_side)) / (s_side - s_star)  //
249                      - fact / (s_side - s_star) * (ds_side - ds_star);
250   CeedScalar denom  = side.U.density * (s_side - u_side);
251   CeedScalar ddenom = side.U.density * (ds_side - du_side) + dside.U.density * (s_side - u_side);
252 
253   StateConservative star = {
254       1.0,
255       {
256         side.Y.velocity[0] + (s_star - u_side) * normal[0],
257         side.Y.velocity[1] + (s_star - u_side) * normal[1],
258         side.Y.velocity[2] + (s_star - u_side) * normal[2],
259         },
260       side.U.E_total / side.U.density  //
261           + (s_star - u_side) * (s_star + side.Y.pressure / denom)
262   };
263   StateConservative dstar = {
264       0.,
265       {
266         dside.Y.velocity[0] + (ds_star - du_side) * normal[0],
267         dside.Y.velocity[1] + (ds_star - du_side) * normal[1],
268         dside.Y.velocity[2] + (ds_star - du_side) * normal[2],
269         },
270       dside.U.E_total / side.U.density - side.U.E_total / Square(side.U.density) * dside.U.density  //
271           + (ds_star - du_side) * (s_star + side.Y.pressure / denom)  //
272           + (s_star - u_side) * (ds_star + dside.Y.pressure / denom - side.Y.pressure / Square(denom) * ddenom)  //
273   };
274 
275   const CeedScalar        a[] = {1, ds_side * fact + s_side * dfact, s_side * fact, -ds_side, -s_side};
276   const StateConservative U[] = {dF_side, star, dstar, side.U, dside.U};
277   return StateConservativeMult(5, a, U);
278 }
279 
280 // HLLC Riemann solver (from Toro's book)
281 CEED_QFUNCTION_HELPER StateConservative RiemannFlux_HLLC(NewtonianIdealGasContext gas, State left, State right, const CeedScalar normal[3]) {
282   StateConservative flux_left  = FluxInviscidDotNormal(gas, left, normal);
283   StateConservative flux_right = FluxInviscidDotNormal(gas, right, normal);
284 
285   CeedScalar u_left  = Dot3(left.Y.velocity, normal);
286   CeedScalar u_right = Dot3(right.Y.velocity, normal);
287   CeedScalar s_left, s_right;
288   ComputeHLLSpeeds_Roe(gas, left, u_left, right, u_right, &s_left, &s_right);
289 
290   // Contact wave speed; Toro (10.37)
291   CeedScalar rhou_left = left.U.density * u_left, rhou_right = right.U.density * u_right;
292   CeedScalar numer  = right.Y.pressure - left.Y.pressure + rhou_left * (s_left - u_left) - rhou_right * (s_right - u_right);
293   CeedScalar denom  = left.U.density * (s_left - u_left) - right.U.density * (s_right - u_right);
294   CeedScalar s_star = numer / denom;
295 
296   // Compute HLLC flux
297   if (0 <= s_left) {
298     return flux_left;
299   } else if (0 <= s_star) {
300     return RiemannFlux_HLLC_Star(gas, left, flux_left, normal, u_left, s_left, s_star);
301   } else if (0 <= s_right) {
302     return RiemannFlux_HLLC_Star(gas, right, flux_right, normal, u_right, s_right, s_star);
303   } else {
304     return flux_right;
305   }
306 }
307 
308 CEED_QFUNCTION_HELPER StateConservative RiemannFlux_HLLC_fwd(NewtonianIdealGasContext gas, State left, State dleft, State right, State dright,
309                                                              const CeedScalar normal[3]) {
310   StateConservative flux_left   = FluxInviscidDotNormal(gas, left, normal);
311   StateConservative flux_right  = FluxInviscidDotNormal(gas, right, normal);
312   StateConservative dflux_left  = FluxInviscidDotNormal_fwd(gas, left, dleft, normal);
313   StateConservative dflux_right = FluxInviscidDotNormal_fwd(gas, right, dright, normal);
314 
315   CeedScalar u_left   = Dot3(left.Y.velocity, normal);
316   CeedScalar u_right  = Dot3(right.Y.velocity, normal);
317   CeedScalar du_left  = Dot3(dleft.Y.velocity, normal);
318   CeedScalar du_right = Dot3(dright.Y.velocity, normal);
319 
320   CeedScalar s_left, ds_left, s_right, ds_right;
321   ComputeHLLSpeeds_Roe_fwd(gas, left, dleft, u_left, du_left, right, dright, u_right, du_right, &s_left, &ds_left, &s_right, &ds_right);
322 
323   // Contact wave speed; Toro (10.37)
324   CeedScalar rhou_left = left.U.density * u_left, drhou_left = left.U.density * du_left + dleft.U.density * u_left;
325   CeedScalar rhou_right = right.U.density * u_right, drhou_right = right.U.density * du_right + dright.U.density * u_right;
326   CeedScalar numer = right.Y.pressure - left.Y.pressure  //
327                      + rhou_left * (s_left - u_left)     //
328                      - rhou_right * (s_right - u_right);
329   CeedScalar dnumer = dright.Y.pressure - dleft.Y.pressure                                //
330                       + rhou_left * (ds_left - du_left) + drhou_left * (s_left - u_left)  //
331                       - rhou_right * (ds_right - du_right) - drhou_right * (s_right - u_right);
332   CeedScalar denom  = left.U.density * (s_left - u_left) - right.U.density * (s_right - u_right);
333   CeedScalar ddenom = left.U.density * (ds_left - du_left) + dleft.U.density * (s_left - u_left)  //
334                       - right.U.density * (ds_right - du_right) - dright.U.density * (s_right - u_right);
335   CeedScalar s_star  = numer / denom;
336   CeedScalar ds_star = dnumer / denom - numer / Square(denom) * ddenom;
337 
338   // Compute HLLC flux
339   if (0 <= s_left) {
340     return dflux_left;
341   } else if (0 <= s_star) {
342     return RiemannFlux_HLLC_Star_fwd(gas, left, dleft, flux_left, dflux_left, normal, u_left, du_left, s_left, ds_left, s_star, ds_star);
343   } else if (0 <= s_right) {
344     return RiemannFlux_HLLC_Star_fwd(gas, right, dright, flux_right, dflux_right, normal, u_right, du_right, s_right, ds_right, s_star, ds_star);
345   } else {
346     return dflux_right;
347   }
348 }
349 
350 #endif  // riemann_solver_h
351