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Definition of the variables to post-process

Additional post-processing variables

For the mesh parts defined using the GUI or in cs_user_postprocess.c, the cs_user_postprocess_values function of the cs_user_postprocess.c file may be used to specify the variables to post-process (called for each postprocess output mesh, at every active time step of an associated writer).

The output of a given variable is generated by means of a call to the cs_post_write_var for cell or face values, cs_post_write_vertex_var for vertex values, \cs_post_write_particle_values for particle or trajectory values, and cs_post_write_probe_values for probe or profile values.

The examples of post-processing given below use meshes defined in the examples for \cs_user_postprocess_meshes above.

Output of the turbulent kinetic energy for the Rij-Epsilon model on the volume mesh

One can define, compute and post-process the turbulent kinetic energy for the Rij-Epsilon as shown in the following example:

if (cat_id == CS_POST_MESH_VOLUME && cs_glob_turb_model->itytur == 3) {
cs_real_t *s_cell;
BFT_MALLOC(s_cell, n_cells, cs_real_t);
const cs_real_6_t *cvar_r = (const cs_real_6_t *)(CS_F_(rij)->val);
for (cs_lnum_t i = 0; i < n_cells; i++) {
cs_lnum_t cell_id = cell_list[i];
s_cell[i] = 0.5* ( cvar_r[cell_id][0]
+ cvar_r[cell_id][1]
+ cvar_r[cell_id][2]);
}
}
else {
const cs_real_t *cvar_r11 = CS_F_(r11)->val;
const cs_real_t *cvar_r22 = CS_F_(r22)->val;
const cs_real_t *cvar_r33 = CS_F_(r33)->val;
for (cs_lnum_t i = 0; i < n_cells; i++) {
cs_lnum_t cell_id = cell_list[i];
s_cell[i] = 0.5* ( cvar_r11[cell_id]
+ cvar_r22[cell_id]
+ cvar_r33[cell_id]);
}
}
CS_POST_WRITER_ALL_ASSOCIATED, /* writer id filter */
"Turb energy", /* var_name */
1, /* var_dim */
true, /* interlace, */
false, /* use_parent */
CS_POST_TYPE_cs_real_t, /* var_type */
s_cell, /* cel_vals */
NULL, /* i_face_vals */
NULL, /* b_face_vals */
ts);
BFT_FREE(s_cell);
}
#define BFT_MALLOC(_ptr, _ni, _type)
Allocate memory for _ni elements of type _type.
Definition bft_mem.h:62
#define BFT_FREE(_ptr)
Free allocated memory.
Definition bft_mem.h:101
double cs_real_t
Floating-point value.
Definition cs_defs.h:302
cs_real_t cs_real_6_t[6]
vector of 6 floating-point values
Definition cs_defs.h:317
int cs_lnum_t
local mesh entity id
Definition cs_defs.h:298
@ r33
Definition cs_field_pointer.h:75
@ rij
Definition cs_field_pointer.h:79
@ r22
Definition cs_field_pointer.h:74
@ r11
Definition cs_field_pointer.h:73
#define CS_F_(e)
Macro used to return a field pointer by its enumerated value.
Definition cs_field_pointer.h:51
void cs_post_write_var(int mesh_id, int writer_id, const char *var_name, int var_dim, bool interlace, bool use_parent, cs_post_type_t var_type, const void *cel_vals, const void *i_face_vals, const void *b_face_vals, const cs_time_step_t *ts)
Output a variable defined at cells or faces of a post-processing mesh using associated writers.
Definition cs_post.c:5080
#define CS_POST_MESH_VOLUME
Definition cs_post.h:75
#define CS_POST_WRITER_ALL_ASSOCIATED
Definition cs_post.h:63
@ CS_POST_TYPE_cs_real_t
Definition cs_post.h:93
const cs_turb_model_t * cs_glob_turb_model
const cs_turb_rans_model_t * cs_glob_turb_rans_model
int itytur
Definition cs_turbulence_model.h:99
int irijco
Definition cs_turbulence_model.h:155

Output of a variable on a surface mesh

Values can also be output on a surface mesh, possibly containing a mix of boundary and internal faces. In the following example, we simply average or project adjacent cell values on faces, but more precise techniques could be used:

if (strcmp(mesh_name, "pressure_surface") == 0) { /* Restrict to this mesh */
cs_real_t *cvar_p = CS_F_(p)->val; /* pressure */
/* Ensure variable is synchronized in parallel or periodic cases;
should already have been done before, repeated for safety */
const cs_mesh_t *m = cs_glob_mesh;
cs_real_t *s_i_faces = NULL, *s_b_faces = NULL;
/* Interior faces */
if (n_i_faces > 0) {
BFT_MALLOC(s_i_faces, n_i_faces, cs_real_t);
for (cs_lnum_t i = 0; i < n_i_faces; i++) {
cs_lnum_t face_id = i_face_list[i];
/* Use unweighted mean of adjacent cell values here */
cs_lnum_t c1 = m->i_face_cells[face_id][0];
cs_lnum_t c2 = m->i_face_cells[face_id][1];
s_i_faces[i] = 0.5 * (cvar_p[c1] + cvar_p[c2]);
}
}
/* Boundary faces */
if (n_b_faces > 0) {
BFT_MALLOC(s_b_faces, n_b_faces, cs_real_t);
for (cs_lnum_t i = 0; i < n_b_faces; i++) {
cs_lnum_t face_id = b_face_list[i];
/* Use adjacent cell value here */
cs_lnum_t cell_id = m->b_face_cells[face_id];
s_b_faces[i] = cvar_p[cell_id];
}
}
CS_POST_WRITER_ALL_ASSOCIATED, /* writer id filter */
"Pressure", /* var_name */
1, /* var_dim */
true, /* interlace, */
false, /* use_parent */
CS_POST_TYPE_cs_real_t, /* var_type */
NULL, /* cel_vals */
s_i_faces, /* i_face_vals */
s_b_faces, /* b_face_vals */
ts);
BFT_FREE(s_i_faces);
BFT_FREE(s_b_faces);
}
@ p
Definition cs_field_pointer.h:67
void cs_mesh_sync_var_scal(cs_real_t *var)
Definition cs_mesh.c:3214
cs_mesh_t * cs_glob_mesh
Definition cs_mesh.h:63
cs_lnum_t * b_face_cells
Definition cs_mesh.h:88
cs_lnum_2_t * i_face_cells
Definition cs_mesh.h:87

Simple output of an existing field or array

For fields or arrays already defined on the full mesh, the "use_parent" option of cs_post_write_var may be used to simply reference the values on the parent (i.e. full) mesh when requesting an output. Note that the example below can also be used with probes or profiles:

if ( cat_id == CS_POST_MESH_VOLUME
|| cat_id == CS_POST_MESH_PROBES) {
const cs_field_t *f = cs_field_by_name_try("my_field");
if (f != NULL)
CS_POST_WRITER_ALL_ASSOCIATED, /* writer id filter */
f->name, /* var_name */
1, /* var_dim */
true, /* interlace, */
true, /* use_parent */
CS_POST_TYPE_cs_real_t, /* var_type */
f->val, /* cel_vals */
NULL, /* i_face_vals */
NULL, /* b_face_vals */
ts);
}
cs_field_t * cs_field_by_name_try(const char *name)
Return a pointer to a field based on its name if present.
Definition cs_field.c:2357
#define CS_POST_MESH_PROBES
Definition cs_post.h:79
Field descriptor.
Definition cs_field.h:124
const char * name
Definition cs_field.h:126
cs_real_t * val
Definition cs_field.h:145

Single output of time-independent values

Finally, a minor modification f the above example shows how it is possible to output time-independent values to a writer also used for time-dependent fields without requiring multiple outputs of those values:

if (cat_id == CS_POST_MESH_VOLUME) {
const cs_field_t *f = cs_field_by_name_try("my_const_field");
if (f != NULL) {
if (ts->nt_cur == ts->nt_prev + 1) { /* before time loop */
cs_time_step_t ts0 = *ts;
ts0.nt_cur = 1; /* Negative time step value implies time-independent */
CS_POST_WRITER_ALL_ASSOCIATED, /* writer id filter */
f->name, /* var_name */
1, /* var_dim */
true, /* interlace, */
true, /* use_parent */
CS_POST_TYPE_cs_real_t, /* var_type */
f->val, /* cel_vals */
NULL, /* i_face_vals */
NULL, /* b_face_vals */
&ts0);
}
}
}
time step descriptor
Definition cs_time_step.h:51
int nt_cur
Definition cs_time_step.h:61

Additional profile variables

The following examples match the advanced profile definitions given in Advanced profile definitions.

The first section is common to both profile series:

const cs_mesh_t *m = cs_glob_mesh;
const cs_real_3_t *cell_cen = (const cs_real_3_t *)mq->cell_cen;
const cs_real_3_t *vel = (const cs_real_3_t *)CS_F_(vel)->val;
const cs_real_t uref2 = uref*uref;
const char *name = cs_probe_set_get_name(probes);
const cs_time_step_t *ts_post = (ts->nt_cur == ts->nt_max) ? NULL : ts;
/* Common variables */
const cs_real_t href = 1.;
cs_real_t cs_real_3_t[3]
vector of 3 floating-point values
Definition cs_defs.h:315
@ vel
Definition cs_field_pointer.h:68
cs_mesh_quantities_t * cs_glob_mesh_quantities
const char * cs_probe_set_get_name(cs_probe_set_t *pset)
Retrieve the name related to a cs_probe_set_t structure.
Definition cs_probe.c:538
const cs_turb_ref_values_t * cs_glob_turb_ref_values
Definition cs_mesh_quantities.h:90
cs_real_t * cell_cen
Definition cs_mesh_quantities.h:92
double uref
Definition cs_turbulence_model.h:110

For the profiles along fixed x, the following code is used. Note that this code's complexity is mainly due to extracting Reynolds stresses for different turbulence models and options. Specific values are then computed for each colum, in the switch statement:

if (strncmp(name, "buicesat", strlen("buicesat")) == 0) {
cs_real_t *val;
BFT_MALLOC(val, n_cells, cs_real_t);
char var_name[64];
/* mean x */
cs_real_t x_sum[] = {0, 0};
for (cs_lnum_t i = 0; i < n_cells; i++) {
cs_lnum_t c_id = cell_list[i];
x_sum[0] += cell_cen[c_id][0];
}
x_sum[1] = n_cells;
cs_real_t xpos = x_sum[0]/x_sum[1];
/* Reynolds stresses */
cs_real_6_t *rij = NULL;
if ( turb_mdl->itytur == 2
|| turb_mdl->itytur == 5
|| turb_mdl->itytur == 6) {
cs_post_evm_reynolds_stresses(interpolation_type,
n_cells,
cell_list,
NULL, /* coords */
rij);
} else if (turb_mdl->itytur == 3 && turb_rans_mdl->irijco == 0) {
for (cs_lnum_t i = 0; i < n_cells; i++) {
cs_lnum_t c_id = cell_list[i];
rij[i][0] = CS_F_(r11)->val[c_id];
rij[i][1] = CS_F_(r22)->val[c_id];
rij[i][2] = CS_F_(r33)->val[c_id];
rij[i][3] = CS_F_(r12)->val[c_id];
rij[i][4] = CS_F_(r23)->val[c_id];
rij[i][5] = CS_F_(r13)->val[c_id];
}
} else if (turb_mdl->itytur == 3) {
cs_real_6_t *cvar_rij = (cs_real_6_t *)CS_F_(rij)->val;
for (cs_lnum_t i = 0; i < n_cells; i++) {
cs_lnum_t c_id = cell_list[i];
for (cs_lnum_t j = 0; j < 6; j++)
rij[i][j] = cvar_rij[c_id][j];
}
}
/* Loop on columns */
for (int col = 0; col < 7; col++) {
switch(col) {
case 0:
{
strncpy(var_name, "U*10+x/h", 64);
for (cs_lnum_t i = 0; i < n_cells; i++) {
cs_lnum_t c_id = cell_list[i];
val[i] = vel[c_id][0]*10 + xpos;
}
}
break;
case 1:
{
strncpy(var_name, "Y/H", 64);
for (cs_lnum_t i = 0; i < n_cells; i++) {
cs_lnum_t c_id = cell_list[i];
val[i] = mq->cell_cen[c_id*3 + 1] / href;
}
}
break;
case 2:
{
strncpy(var_name, "U/Uc", 64);
for (cs_lnum_t i = 0; i < n_cells; i++) {
cs_lnum_t c_id = cell_list[i];
val[i] = vel[c_id][0] / uref;
}
}
break;
case 3:
{
strncpy(var_name, "uu/Uc^2", 64);
for (cs_lnum_t i = 0; i < n_cells; i++) {
val[i] = rij[i][0] / uref2;
}
}
break;
case 4:
{
strncpy(var_name, "uv/Uc^2", 64);
for (cs_lnum_t i = 0; i < n_cells; i++) {
val[i] = rij[i][3] / uref2;
}
}
break;
case 5:
{
strncpy(var_name, "vv/Uc^2", 64);
for (cs_lnum_t i = 0; i < n_cells; i++) {
val[i] = rij[i][1] / uref2;
}
}
break;
case 6:
{
strncpy(var_name, "X", 64);
for (cs_lnum_t i = 0; i < n_cells; i++) {
cs_lnum_t c_id = cell_list[i];
val[i] = cell_cen[c_id][0];
}
}
break;
}
(mesh_id,
CS_POST_WRITER_ALL_ASSOCIATED, /* writer id filter */
var_name, /* var_name */
1, /* var_dim */
0, /* parent location id */
NULL, /* default interpolation */
NULL, /* interpolation input */
val,
ts_post);
}
BFT_FREE(val);
}
#define CS_REAL_TYPE
Definition cs_defs.h:407
cs_field_interpolate_t
Definition cs_field_operator.h:54
@ CS_FIELD_INTERPOLATE_MEAN
Definition cs_field_operator.h:56
@ r13
Definition cs_field_pointer.h:78
@ r23
Definition cs_field_pointer.h:77
@ r12
Definition cs_field_pointer.h:76
static void cs_parall_sum(int n, cs_datatype_t datatype, void *val)
Sum values of a given datatype on all default communicator processes.
Definition cs_parall.h:147
void cs_post_write_probe_values(int mesh_id, int writer_id, const char *var_name, int var_dim, cs_post_type_t var_type, int parent_location_id, cs_interpolate_from_location_t *interpolate_func, void *interpolate_input, const void *vals, const cs_time_step_t *ts)
Output a variable defined at cells or faces of a post-processing mesh using associated writers.
Definition cs_post.c:5619
void cs_post_evm_reynolds_stresses(cs_field_interpolate_t interpolation_type, cs_lnum_t n_cells, const cs_lnum_t cell_ids[], const cs_real_3_t *coords, cs_real_6_t *rst)
Compute Reynolds stresses in case of Eddy Viscosity Models.
Definition cs_post_util.c:720
double precision, dimension(:,:), allocatable xpos
Positions.
Definition atimbr.f90:103
real(c_double), pointer, save uref
the characteristic flow velocity, used for the initialization of the turbulence. Negative value: not ...
Definition cstphy.f90:619
Turbulence model general options descriptor.
Definition cs_turbulence_model.h:75
RANS turbulence model descriptor.
Definition cs_turbulence_model.h:117

For the profile defined all around a foil, the following code is used to compute the pressure coefficient and output its values:

const cs_mesh_t *m = cs_glob_mesh;
const cs_real_3_t *b_face_cog = (const cs_real_3_t *)mq->b_face_cog;
cs_real_t * b_face_cog
Definition cs_mesh_quantities.h:105
cs_real_t *val;
BFT_MALLOC(val, n_b_faces, cs_real_t);
/* x coordinate */
for (cs_lnum_t i = 0; i < n_b_faces; i++) {
cs_lnum_t face_id = b_face_list[i];
val[i] = b_face_cog[face_id][0];
}
/* post-process x coordinate */
(mesh_id,
CS_POST_WRITER_ALL_ASSOCIATED, /* writer id filter */
"X", /* var_name */
1, /* var_dim */
0, /* parent location id */
NULL, /* default interpolation */
NULL, /* interpolation input */
val,
ts);
/* compute pressure on selected boundary faces */
cs_post_b_pressure(n_b_faces, b_face_list, val);
cs_real_t p0 = phys_pro->p0; /* reference pressure */
cs_real_t ro0 = phys_pro->ro0; /* reference density */
const cs_real_t uref = cs_glob_turb_ref_values->uref; /*ref. velocity */
const cs_real_t uref2 = uref*uref;
/* reference values can be set in GUI */
/* 1/(1/2 rho U^2) */
cs_real_t div_half_ro0_uref2 = 1. / (0.5 * ro0 * uref2);
/* compute CP at each selected boundary face */
for (cs_lnum_t i = 0; i < n_b_faces; i++)
val[i] = (val[i] - p0) * div_half_ro0_uref2;
/* post-process CP */
(mesh_id,
CS_POST_WRITER_ALL_ASSOCIATED, /* writer id filter */
"CP", /* var_name */
1, /* var_dim */
0, /* parent location id */
NULL, /* default interpolation */
NULL, /* interpolation input */
val,
ts);
BFT_FREE(val);
cs_fluid_properties_t * cs_get_glob_fluid_properties(void)
Definition cs_physical_constants.c:524
void cs_post_b_pressure(cs_lnum_t n_b_faces, const cs_lnum_t b_face_ids[], cs_real_t pres[])
Compute pressure on a specific boundary region.
Definition cs_post_util.c:633
Fluid properties descriptor.
Definition cs_physical_constants.h:61
double ro0
Definition cs_physical_constants.h:72
double p0
Definition cs_physical_constants.h:74

For the last profiles series, values for each column are also computed, requiring a reference pressure based on the mesh point closest to a given point, and computation of tangential stresses, so as to determine drag coefficients.

else if ( strcmp(name, "buicstr") == 0
|| strcmp(name, "buicinc") == 0) {
const cs_lnum_t *b_face_cells = m->b_face_cells;
const cs_real_3_t *face_cog = (const cs_real_3_t *)mq->b_face_cog;
const cs_real_t *distb = mq->b_dist;
const cs_real_t *pres = CS_F_(p)->val;
cs_real_t div_half_ro0_uref2 = 1. / (0.5 * phys_pro->ro0 * uref2);
cs_real_t *val;
BFT_MALLOC(val, n_b_faces, cs_real_t);
char var_name[64];
/* Reference pressure */
cs_real_t xyz_ref[3] = {-1.7, -0.5, 0.005};
cs_real_t pref = 0;
cs_lnum_t pref_id;
int pref_rank;
(const cs_real_3_t *)(mq->cell_cen),
xyz_ref,
&pref_id,
&pref_rank);
if (pref_rank == cs_glob_rank_id)
pref = pres[pref_id];
cs_parall_bcast(pref_rank, 1, CS_REAL_TYPE, &pref);
/* Stresses */
cs_real_3_t *stresses;
BFT_MALLOC(stresses, n_b_faces, cs_real_3_t);
cs_post_stress_tangential(n_b_faces, b_face_list, stresses);
/* Loop on columns */
for (int col = 0; col < 5; col++) {
switch(col) {
case 0:
{
strncpy(var_name, "X/H", 64);
for (cs_lnum_t i = 0; i < n_b_faces; i++) {
cs_lnum_t f_id = b_face_list[i];
val[i] = face_cog[f_id][0] / href;
}
}
break;
case 1:
{
strncpy(var_name, "CP", 64);
for (cs_lnum_t i = 0; i < n_b_faces; i++) {
cs_lnum_t f_id = b_face_list[i];
cs_lnum_t c_id = b_face_cells[f_id];
val[i] = (pres[c_id] - pref) * div_half_ro0_uref2;
}
}
break;
case 2:
{
strncpy(var_name, "CF", 64);
for (cs_lnum_t i = 0; i < n_b_faces; i++) {
val[i] = cs_math_3_norm(stresses[i]) * div_half_ro0_uref2;
}
}
break;
case 3:
{
strncpy(var_name, "U/UREF", 64);
for (cs_lnum_t i = 0; i < n_b_faces; i++) {
/* previous value in val[i] from case2:
norm(stresses[i])/(0.5.ro0.uref^2) */
val[i] = copysign(val[i], stresses[i][0]);
}
}
break;
case 4:
{
strncpy(var_name, "YPLUS", 64);
for (cs_lnum_t i = 0; i < n_b_faces; i++) {
cs_lnum_t f_id = b_face_list[i];
cs_lnum_t c_id = b_face_cells[f_id];
val[i] = sqrt(fabs(vel[c_id][0])*distb[f_id]*phys_pro->viscl0);
}
}
break;
}
(mesh_id,
CS_POST_WRITER_ALL_ASSOCIATED, /* writer id filter */
var_name, /* var_name */
1, /* var_dim */
0, /* parent location id */
NULL, /* default interpolation */
NULL, /* interpolation input */
val,
ts_post);
}
BFT_FREE(stresses);
BFT_FREE(val);
}
int cs_glob_rank_id
Definition cs_defs.c:176
void cs_geom_closest_point(cs_lnum_t n_points, const cs_real_t point_coords[][3], const cs_real_t query_coords[3], cs_lnum_t *point_id, int *rank_id)
find the closest point of a set to a given point in space.
Definition cs_geom.c:162
static cs_real_t cs_math_3_norm(const cs_real_t v[3])
Compute the euclidean norm of a vector of dimension 3.
Definition cs_math.h:372
static void cs_parall_bcast(int root_rank, int n, cs_datatype_t datatype, void *val)
Broadcast values of a given datatype to all default communicator processes.
Definition cs_parall.h:255
void cs_post_stress_tangential(cs_lnum_t n_b_faces, const cs_lnum_t b_face_ids[], cs_real_3_t stress[])
Compute tangential stress on a specific boundary.
Definition cs_post_util.c:592
double viscl0
Definition cs_physical_constants.h:73
cs_lnum_t n_cells
Definition cs_mesh.h:73