xref: /libCEED/examples/fluids/qfunctions/advection.h (revision 76f753ba08291aebcf5daab54b10d67cec446c40)
1 // Copyright (c) 2017-2024, 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 /// Advection initial condition and operator for Navier-Stokes example using PETSc
10 #include <ceed.h>
11 #include <math.h>
12 
13 #include "advection_types.h"
14 #include "newtonian_state.h"
15 #include "newtonian_types.h"
16 #include "stabilization_types.h"
17 #include "utils.h"
18 
19 // *****************************************************************************
20 // This QFunction sets the initial conditions and the boundary conditions
21 //   for two test cases: ROTATION and TRANSLATION
22 //
23 // -- ROTATION (default)
24 //      Initial Conditions:
25 //        Mass Density:
26 //          Constant mass density of 1.0
27 //        Momentum Density:
28 //          Rotational field in x,y
29 //        Energy Density:
30 //          Maximum of 1. x0 decreasing linearly to 0. as radial distance
31 //            increases to (1.-r/rc), then 0. everywhere else
32 //
33 //      Boundary Conditions:
34 //        Mass Density:
35 //          0.0 flux
36 //        Momentum Density:
37 //          0.0
38 //        Energy Density:
39 //          0.0 flux
40 //
41 // -- TRANSLATION
42 //      Initial Conditions:
43 //        Mass Density:
44 //          Constant mass density of 1.0
45 //        Momentum Density:
46 //           Constant rectilinear field in x,y
47 //        Energy Density:
48 //          Maximum of 1. x0 decreasing linearly to 0. as radial distance
49 //            increases to (1.-r/rc), then 0. everywhere else
50 //
51 //      Boundary Conditions:
52 //        Mass Density:
53 //          0.0 flux
54 //        Momentum Density:
55 //          0.0
56 //        Energy Density:
57 //          Inflow BCs:
58 //            E = E_wind
59 //          Outflow BCs:
60 //            E = E(boundary)
61 //          Both In/Outflow BCs for E are applied weakly in the
62 //            QFunction "Advection2d_Sur"
63 //
64 // *****************************************************************************
65 
66 // *****************************************************************************
67 // This helper function provides the exact, time-dependent solution and IC formulation for 2D advection
68 // *****************************************************************************
69 CEED_QFUNCTION_HELPER CeedInt Exact_AdvectionGeneric(CeedInt dim, CeedScalar time, const CeedScalar X[], CeedInt Nf, CeedScalar q[], void *ctx) {
70   const SetupContextAdv context = (SetupContextAdv)ctx;
71   const CeedScalar      rc      = context->rc;
72   const CeedScalar      lx      = context->lx;
73   const CeedScalar      ly      = context->ly;
74   const CeedScalar      lz      = dim == 2 ? 0. : context->lz;
75   const CeedScalar     *wind    = context->wind;
76 
77   const CeedScalar center[3] = {0.5 * lx, 0.5 * ly, 0.5 * lz};
78   const CeedScalar theta     = dim == 2 ? M_PI / 3 : M_PI;
79   const CeedScalar x0[3]     = {center[0] + .25 * lx * cos(theta + time), center[1] + .25 * ly * sin(theta + time), 0.5 * lz};
80 
81   const CeedScalar x = X[0], y = X[1], z = dim == 2 ? 0. : X[2];
82 
83   CeedScalar r = 0.;
84   switch (context->initial_condition_type) {
85     case ADVECTIONIC_BUBBLE_SPHERE:
86     case ADVECTIONIC_BUBBLE_CYLINDER:
87       r = sqrt(Square(x - x0[0]) + Square(y - x0[1]) + Square(z - x0[2]));
88       break;
89     case ADVECTIONIC_COSINE_HILL:
90       r = sqrt(Square(x - center[0]) + Square(y - center[1]));
91       break;
92     case ADVECTIONIC_SKEW:
93       break;
94   }
95 
96   switch (context->wind_type) {
97     case WIND_ROTATION:
98       q[0] = 1.;
99       q[1] = -(y - center[1]);
100       q[2] = (x - center[0]);
101       q[3] = 0;
102       break;
103     case WIND_TRANSLATION:
104       q[0] = 1.;
105       q[1] = wind[0];
106       q[2] = wind[1];
107       q[3] = dim == 2 ? 0. : wind[2];
108       break;
109     default:
110       return 1;
111   }
112 
113   switch (context->initial_condition_type) {
114     case ADVECTIONIC_BUBBLE_SPHERE:
115     case ADVECTIONIC_BUBBLE_CYLINDER:
116       switch (context->bubble_continuity_type) {
117         // original continuous, smooth shape
118         case BUBBLE_CONTINUITY_SMOOTH:
119           q[4] = r <= rc ? (1. - r / rc) : 0.;
120           break;
121         // discontinuous, sharp back half shape
122         case BUBBLE_CONTINUITY_BACK_SHARP:
123           q[4] = ((r <= rc) && (y < center[1])) ? (1. - r / rc) : 0.;
124           break;
125         // attempt to define a finite thickness that will get resolved under grid refinement
126         case BUBBLE_CONTINUITY_THICK:
127           q[4] = ((r <= rc) && (y < center[1])) ? (1. - r / rc) * fmin(1.0, (center[1] - y) / 1.25) : 0.;
128           break;
129         case BUBBLE_CONTINUITY_COSINE:
130           q[4] = r <= rc ? .5 + .5 * cos(r * M_PI / rc) : 0;
131           break;
132       }
133       break;
134     case ADVECTIONIC_COSINE_HILL: {
135       CeedScalar half_width = context->lx / 2;
136       q[4]                  = r > half_width ? 0. : cos(2 * M_PI * r / half_width + M_PI) + 1.;
137     } break;
138     case ADVECTIONIC_SKEW: {
139       CeedScalar       skewed_barrier[3]  = {wind[0], wind[1], 0};
140       CeedScalar       inflow_to_point[3] = {x - context->lx / 2, y, 0};
141       CeedScalar       cross_product[3]   = {0};
142       const CeedScalar boundary_threshold = 20 * CEED_EPSILON;
143       Cross3(skewed_barrier, inflow_to_point, cross_product);
144 
145       q[4] = cross_product[2] > boundary_threshold ? 0 : 1;
146       if ((x < boundary_threshold && wind[0] < boundary_threshold) ||                // outflow at -x boundary
147           (y < boundary_threshold && wind[1] < boundary_threshold) ||                // outflow at -y boundary
148           (x > context->lx - boundary_threshold && wind[0] > boundary_threshold) ||  // outflow at +x boundary
149           (y > context->ly - boundary_threshold && wind[1] > boundary_threshold)     // outflow at +y boundary
150       ) {
151         q[4] = 0;
152       }
153     } break;
154   }
155   return 0;
156 }
157 
158 // *****************************************************************************
159 // This QFunction sets the initial conditions for 3D advection
160 // *****************************************************************************
161 CEED_QFUNCTION(ICsAdvection)(void *ctx, CeedInt Q, const CeedScalar *const *in, CeedScalar *const *out) {
162   const CeedScalar(*X)[CEED_Q_VLA] = (const CeedScalar(*)[CEED_Q_VLA])in[0];
163   CeedScalar(*q0)[CEED_Q_VLA]      = (CeedScalar(*)[CEED_Q_VLA])out[0];
164 
165   CeedPragmaSIMD for (CeedInt i = 0; i < Q; i++) {
166     const CeedScalar x[]  = {X[0][i], X[1][i], X[2][i]};
167     CeedScalar       q[5] = {0.};
168 
169     Exact_AdvectionGeneric(3, 0., x, 5, q, ctx);
170     for (CeedInt j = 0; j < 5; j++) q0[j][i] = q[j];
171   }
172   return 0;
173 }
174 
175 // *****************************************************************************
176 // This QFunction sets the initial conditions for 2D advection
177 // *****************************************************************************
178 CEED_QFUNCTION(ICsAdvection2d)(void *ctx, CeedInt Q, const CeedScalar *const *in, CeedScalar *const *out) {
179   const CeedScalar(*X)[CEED_Q_VLA] = (const CeedScalar(*)[CEED_Q_VLA])in[0];
180   CeedScalar(*q0)[CEED_Q_VLA]      = (CeedScalar(*)[CEED_Q_VLA])out[0];
181   const SetupContextAdv context    = (SetupContextAdv)ctx;
182 
183   CeedPragmaSIMD for (CeedInt i = 0; i < Q; i++) {
184     const CeedScalar x[]  = {X[0][i], X[1][i]};
185     CeedScalar       q[5] = {0.};
186 
187     Exact_AdvectionGeneric(2, context->time, x, 5, q, ctx);
188     for (CeedInt j = 0; j < 5; j++) q0[j][i] = q[j];
189   }
190   return 0;
191 }
192 
193 CEED_QFUNCTION_HELPER void QdataUnpack_ND(CeedInt N, CeedInt Q, CeedInt i, const CeedScalar *q_data, CeedScalar *wdetJ, CeedScalar *dXdx) {
194   // Cannot directly use QdataUnpack* helper functions due to SYCL online compiler incompatabilities
195   switch (N) {
196     case 2:
197       StoredValuesUnpack(Q, i, 0, 1, q_data, wdetJ);
198       StoredValuesUnpack(Q, i, 1, 4, q_data, dXdx);
199       break;
200     case 3:
201       StoredValuesUnpack(Q, i, 0, 1, q_data, wdetJ);
202       StoredValuesUnpack(Q, i, 1, 9, q_data, dXdx);
203       break;
204   }
205 }
206 
207 CEED_QFUNCTION_HELPER int QdataBoundaryUnpack_ND(CeedInt N, CeedInt Q, CeedInt i, const CeedScalar *q_data, CeedScalar *wdetJ, CeedScalar *dXdx,
208                                                  CeedScalar *normal) {
209   // Cannot directly use QdataBoundaryUnpack* helper functions due to SYCL online compiler incompatabilities
210   switch (N) {
211     case 2:
212       if (wdetJ) StoredValuesUnpack(Q, i, 0, 1, q_data, wdetJ);
213       if (normal) StoredValuesUnpack(Q, i, 1, 2, q_data, normal);
214       break;
215     case 3:
216       if (wdetJ) StoredValuesUnpack(Q, i, 0, 1, q_data, wdetJ);
217       if (normal) StoredValuesUnpack(Q, i, 1, 3, q_data, normal);
218       if (dXdx) StoredValuesUnpack(Q, i, 4, 6, q_data, (CeedScalar *)dXdx);
219       break;
220   }
221   return CEED_ERROR_SUCCESS;
222 }
223 
224 CEED_QFUNCTION_HELPER void StatePhysicalGradientFromReference_ND(CeedInt N, CeedInt Q, CeedInt i, NewtonianIdealGasContext gas, State s,
225                                                                  StateVariable state_var, const CeedScalar *grad_q, const CeedScalar *dXdx,
226                                                                  State *grad_s) {
227   switch (N) {
228     case 2: {
229       for (CeedInt k = 0; k < 2; k++) {
230         CeedScalar dqi[5];
231         for (CeedInt j = 0; j < 5; j++) {
232           dqi[j] = grad_q[(Q * 5) * 0 + Q * j + i] * dXdx[0 * N + k] + grad_q[(Q * 5) * 1 + Q * j + i] * dXdx[1 * N + k];
233         }
234         grad_s[k] = StateFromQ_fwd(gas, s, dqi, state_var);
235       }
236       CeedScalar U[5] = {0.};
237       grad_s[2]       = StateFromU(gas, U);
238     } break;
239     case 3:
240       // Cannot directly use StatePhysicalGradientFromReference helper functions due to SYCL online compiler incompatabilities
241       for (CeedInt k = 0; k < 3; k++) {
242         CeedScalar dqi[5];
243         for (CeedInt j = 0; j < 5; j++) {
244           dqi[j] = grad_q[(Q * 5) * 0 + Q * j + i] * dXdx[0 * N + k] + grad_q[(Q * 5) * 1 + Q * j + i] * dXdx[1 * N + k] +
245                    grad_q[(Q * 5) * 2 + Q * j + i] * dXdx[2 * N + k];
246         }
247         grad_s[k] = StateFromQ_fwd(gas, s, dqi, state_var);
248       }
249       break;
250   }
251 }
252 
253 // *****************************************************************************
254 // This QFunction implements Advection for implicit time stepping method
255 // *****************************************************************************
256 CEED_QFUNCTION_HELPER void IFunction_AdvectionGeneric(void *ctx, CeedInt Q, const CeedScalar *const *in, CeedScalar *const *out, CeedInt dim) {
257   const CeedScalar(*q)[CEED_Q_VLA]     = (const CeedScalar(*)[CEED_Q_VLA])in[0];
258   const CeedScalar(*grad_q)            = in[1];
259   const CeedScalar(*q_dot)[CEED_Q_VLA] = (const CeedScalar(*)[CEED_Q_VLA])in[2];
260   const CeedScalar(*q_data)            = in[3];
261 
262   CeedScalar(*v)[CEED_Q_VLA]         = (CeedScalar(*)[CEED_Q_VLA])out[0];
263   CeedScalar(*grad_v)[5][CEED_Q_VLA] = (CeedScalar(*)[5][CEED_Q_VLA])out[1];
264   CeedScalar *jac_data               = out[2];
265 
266   AdvectionContext                 context   = (AdvectionContext)ctx;
267   const CeedScalar                 CtauS     = context->CtauS;
268   const CeedScalar                 zeros[14] = {0.};
269   NewtonianIdealGasContext         gas;
270   struct NewtonianIdealGasContext_ gas_struct = {0};
271   gas                                         = &gas_struct;
272 
273   CeedPragmaSIMD for (CeedInt i = 0; i < Q; i++) {
274     const CeedScalar qi[5] = {q[0][i], q[1][i], q[2][i], q[3][i], q[4][i]};
275     const State      s     = StateFromU(gas, qi);
276 
277     CeedScalar wdetJ, dXdx[9];
278     QdataUnpack_ND(dim, Q, i, q_data, &wdetJ, dXdx);
279     State grad_s[3];
280     StatePhysicalGradientFromReference_ND(dim, Q, i, gas, s, STATEVAR_CONSERVATIVE, grad_q, dXdx, grad_s);
281 
282     const CeedScalar Grad_E[3] = {grad_s[0].U.E_total, grad_s[1].U.E_total, grad_s[2].U.E_total};
283 
284     for (CeedInt f = 0; f < 4; f++) {
285       for (CeedInt j = 0; j < dim; j++) grad_v[j][f][i] = 0;  // No Change in density or momentum
286       v[f][i] = wdetJ * q_dot[f][i];                          // K Mass/transient term
287     }
288 
289     CeedScalar div_u = 0;
290     for (CeedInt j = 0; j < dim; j++) {
291       for (CeedInt k = 0; k < dim; k++) {
292         div_u += grad_s[k].Y.velocity[j];
293       }
294     }
295     CeedScalar strong_conv = s.U.E_total * div_u + DotN(s.Y.velocity, Grad_E, dim);
296     CeedScalar strong_res  = q_dot[4][i] + strong_conv;
297 
298     v[4][i] = wdetJ * q_dot[4][i];  // transient part (ALWAYS)
299 
300     CeedScalar uX[3] = {0.};
301     MatVecNM(dXdx, s.Y.velocity, dim, dim, CEED_NOTRANSPOSE, uX);
302 
303     if (context->strong_form) {  // Strong Galerkin convection term: v div(E u)
304       v[4][i] += wdetJ * strong_conv;
305     } else {  // Weak Galerkin convection term: -dv \cdot (E u)
306       for (CeedInt j = 0; j < dim; j++) grad_v[j][4][i] = -wdetJ * s.U.E_total * uX[j];
307     }
308 
309     CeedScalar TauS = 0;
310     switch (context->stabilization_tau) {
311       case STAB_TAU_CTAU:
312         TauS = CtauS / sqrt(Dot3(uX, uX));
313         break;
314       case STAB_TAU_ADVDIFF_SHAKIB: {
315         CeedScalar gijd_mat[9] = {0.}, gij_uj[3] = {0.};
316         MatMatN(dXdx, dXdx, dim, CEED_TRANSPOSE, CEED_NOTRANSPOSE, gijd_mat);
317 
318         MatVecNM(gijd_mat, s.Y.velocity, dim, dim, CEED_NOTRANSPOSE, gij_uj);
319         TauS = 1 / sqrt(Square(2 * context->Ctau_t / context->dt) + DotN(s.Y.velocity, gij_uj, dim) * context->Ctau_a);
320       } break;
321     }
322 
323     for (CeedInt j = 0; j < dim; j++) switch (context->stabilization) {
324         case STAB_NONE:
325           break;
326         case STAB_SU:
327           grad_v[j][4][i] += wdetJ * TauS * strong_conv * uX[j];
328           break;
329         case STAB_SUPG:
330           grad_v[j][4][i] += wdetJ * TauS * strong_res * uX[j];
331           break;
332       }
333     StoredValuesPack(Q, i, 0, 14, zeros, jac_data);
334   }
335 }
336 
337 CEED_QFUNCTION(IFunction_Advection)(void *ctx, CeedInt Q, const CeedScalar *const *in, CeedScalar *const *out) {
338   IFunction_AdvectionGeneric(ctx, Q, in, out, 3);
339   return 0;
340 }
341 
342 CEED_QFUNCTION(IFunction_Advection2d)(void *ctx, CeedInt Q, const CeedScalar *const *in, CeedScalar *const *out) {
343   IFunction_AdvectionGeneric(ctx, Q, in, out, 2);
344   return 0;
345 }
346 
347 // *****************************************************************************
348 // This QFunction implements Advection for explicit time stepping method
349 // *****************************************************************************
350 CEED_QFUNCTION_HELPER void RHSFunction_AdvectionGeneric(void *ctx, CeedInt Q, const CeedScalar *const *in, CeedScalar *const *out, CeedInt dim) {
351   const CeedScalar(*q)[CEED_Q_VLA] = (const CeedScalar(*)[CEED_Q_VLA])in[0];
352   const CeedScalar(*grad_q)        = in[1];
353   const CeedScalar(*q_data)        = in[2];
354 
355   CeedScalar(*v)[CEED_Q_VLA]         = (CeedScalar(*)[CEED_Q_VLA])out[0];
356   CeedScalar(*grad_v)[5][CEED_Q_VLA] = (CeedScalar(*)[5][CEED_Q_VLA])out[1];
357 
358   AdvectionContext                 context = (AdvectionContext)ctx;
359   const CeedScalar                 CtauS   = context->CtauS;
360   NewtonianIdealGasContext         gas;
361   struct NewtonianIdealGasContext_ gas_struct = {0};
362   gas                                         = &gas_struct;
363 
364   CeedPragmaSIMD for (CeedInt i = 0; i < Q; i++) {
365     const CeedScalar qi[5] = {q[0][i], q[1][i], q[2][i], q[3][i], q[4][i]};
366     const State      s     = StateFromU(gas, qi);
367 
368     CeedScalar wdetJ, dXdx[9];
369     QdataUnpack_ND(dim, Q, i, q_data, &wdetJ, dXdx);
370     State grad_s[3];
371     StatePhysicalGradientFromReference_ND(dim, Q, i, gas, s, STATEVAR_CONSERVATIVE, grad_q, dXdx, grad_s);
372 
373     const CeedScalar Grad_E[3] = {grad_s[0].U.E_total, grad_s[1].U.E_total, grad_s[2].U.E_total};
374 
375     for (CeedInt f = 0; f < 4; f++) {
376       for (CeedInt j = 0; j < dim; j++) grad_v[j][f][i] = 0;  // No Change in density or momentum
377       v[f][i] = 0.;
378     }
379 
380     CeedScalar div_u = 0;
381     for (CeedInt j = 0; j < dim; j++) {
382       for (CeedInt k = 0; k < dim; k++) {
383         div_u += grad_s[k].Y.velocity[j];
384       }
385     }
386     CeedScalar strong_conv = s.U.E_total * div_u + DotN(s.Y.velocity, Grad_E, dim);
387 
388     CeedScalar uX[3] = {0.};
389     MatVecNM(dXdx, s.Y.velocity, dim, dim, CEED_NOTRANSPOSE, uX);
390 
391     if (context->strong_form) {  // Strong Galerkin convection term: v div(E u)
392       v[4][i] = -wdetJ * strong_conv;
393       for (CeedInt j = 0; j < dim; j++) grad_v[j][4][i] = 0;
394     } else {  // Weak Galerkin convection term: -dv \cdot (E u)
395       for (CeedInt j = 0; j < dim; j++) grad_v[j][4][i] = wdetJ * s.U.E_total * uX[j];
396       v[4][i] = 0.;
397     }
398 
399     const CeedScalar TauS = CtauS / sqrt(Dot3(uX, uX));
400     for (CeedInt j = 0; j < dim; j++) switch (context->stabilization) {
401         case STAB_NONE:
402           break;
403         case STAB_SU:
404         case STAB_SUPG:
405           grad_v[j][4][i] -= wdetJ * TauS * strong_conv * uX[j];
406           break;
407       }
408   }
409 }
410 
411 CEED_QFUNCTION(RHS_Advection)(void *ctx, CeedInt Q, const CeedScalar *const *in, CeedScalar *const *out) {
412   RHSFunction_AdvectionGeneric(ctx, Q, in, out, 3);
413   return 0;
414 }
415 
416 CEED_QFUNCTION(RHS_Advection2d)(void *ctx, CeedInt Q, const CeedScalar *const *in, CeedScalar *const *out) {
417   RHSFunction_AdvectionGeneric(ctx, Q, in, out, 2);
418   return 0;
419 }
420 
421 // *****************************************************************************
422 // This QFunction implements consistent outflow and inflow BCs
423 //      for advection
424 //
425 //  Inflow and outflow faces are determined based on sign(dot(wind, normal)):
426 //    sign(dot(wind, normal)) > 0 : outflow BCs
427 //    sign(dot(wind, normal)) < 0 : inflow BCs
428 //
429 //  Outflow BCs:
430 //    The validity of the weak form of the governing equations is extended to the outflow and the current values of E are applied.
431 //
432 //  Inflow BCs:
433 //    A prescribed Total Energy (E_wind) is applied weakly.
434 // *****************************************************************************
435 CEED_QFUNCTION(Advection_InOutFlowGeneric)(void *ctx, CeedInt Q, const CeedScalar *const *in, CeedScalar *const *out, CeedInt dim) {
436   const CeedScalar(*q)[CEED_Q_VLA] = (const CeedScalar(*)[CEED_Q_VLA])in[0];
437   const CeedScalar(*q_data_sur)    = in[2];
438 
439   CeedScalar(*v)[CEED_Q_VLA]   = (CeedScalar(*)[CEED_Q_VLA])out[0];
440   AdvectionContext context     = (AdvectionContext)ctx;
441   const CeedScalar E_wind      = context->E_wind;
442   const CeedScalar strong_form = context->strong_form;
443   const bool       is_implicit = context->implicit;
444 
445   CeedPragmaSIMD for (CeedInt i = 0; i < Q; i++) {
446     const CeedScalar rho  = q[0][i];
447     const CeedScalar u[3] = {q[1][i] / rho, q[2][i] / rho, q[3][i] / rho};
448     const CeedScalar E    = q[4][i];
449 
450     CeedScalar wdetJb, norm[3];
451     QdataBoundaryUnpack_ND(dim, Q, i, q_data_sur, &wdetJb, NULL, norm);
452     wdetJb *= is_implicit ? -1. : 1.;
453 
454     const CeedScalar u_normal = DotN(norm, u, dim);
455 
456     // No Change in density or momentum
457     for (CeedInt j = 0; j < 4; j++) {
458       v[j][i] = 0;
459     }
460     // Implementing in/outflow BCs
461     if (u_normal > 0) {  // outflow
462       v[4][i] = -(1 - strong_form) * wdetJb * E * u_normal;
463     } else {  // inflow
464       v[4][i] = -(1 - strong_form) * wdetJb * E_wind * u_normal;
465     }
466   }
467   return 0;
468 }
469 
470 CEED_QFUNCTION(Advection_InOutFlow)(void *ctx, CeedInt Q, const CeedScalar *const *in, CeedScalar *const *out) {
471   Advection_InOutFlowGeneric(ctx, Q, in, out, 3);
472   return 0;
473 }
474 
475 CEED_QFUNCTION(Advection2d_InOutFlow)(void *ctx, CeedInt Q, const CeedScalar *const *in, CeedScalar *const *out) {
476   Advection_InOutFlowGeneric(ctx, Q, in, out, 2);
477   return 0;
478 }
479