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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:
s_cell[i] = 0.5* ( cvar_r[cell_id][0]
+ cvar_r[cell_id][1]
+ cvar_r[cell_id][2]);
}
}
else {
s_cell[i] = 0.5* ( cvar_r11[cell_id]
+ cvar_r22[cell_id]
+ cvar_r33[cell_id]);
}
}
"Turb energy",
1,
true,
false,
s_cell,
NULL,
NULL,
}
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) {
cs_real_t *s_i_faces = NULL, *s_b_faces = NULL;
if (n_i_faces > 0) {
s_i_faces[i] = 0.5 * (cvar_p[
c1] + cvar_p[
c2]);
}
}
if (n_b_faces > 0) {
s_b_faces[i] = cvar_p[cell_id];
}
}
"Pressure",
1,
true,
false,
NULL,
s_i_faces,
s_b_faces,
}
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 (f != NULL)
1,
true,
true,
NULL,
NULL,
}
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 (f != NULL) {
if (
ts->nt_cur ==
ts->nt_prev + 1) {
1,
true,
true,
NULL,
NULL,
&ts0);
}
}
}
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:
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) {
char var_name[64];
x_sum[0] += cell_cen[c_id][0];
}
x_sum[1] = n_cells;
n_cells,
cell_list,
NULL,
}
else if (turb_mdl->
itytur == 3 && turb_rans_mdl->
irijco == 0) {
}
}
else if (turb_mdl->
itytur == 3) {
rij[i][j] = cvar_rij[c_id][j];
}
}
for (int col = 0; col < 7; col++) {
switch(col) {
case 0:
{
strncpy(var_name, "U*10+x/h", 64);
}
}
break;
case 1:
{
strncpy(var_name, "Y/H", 64);
val[i] = mq->
cell_cen[c_id*3 + 1] / href;
}
}
break;
case 2:
{
strncpy(var_name, "U/Uc", 64);
}
}
break;
case 3:
{
strncpy(var_name, "uu/Uc^2", 64);
val[i] =
rij[i][0] / uref2;
}
}
break;
case 4:
{
strncpy(var_name, "uv/Uc^2", 64);
val[i] =
rij[i][3] / uref2;
}
}
break;
case 5:
{
strncpy(var_name, "vv/Uc^2", 64);
val[i] =
rij[i][1] / uref2;
}
}
break;
case 6:
{
strncpy(var_name, "X", 64);
val[i] = cell_cen[c_id][0];
}
}
break;
}
(mesh_id,
var_name,
1,
0,
NULL,
NULL,
val,
ts_post);
}
}
For the profile defined all around a foil, the following code is used to compute the pressure coefficient and output its values:
val[i] = b_face_cog[face_id][0];
}
(mesh_id,
"X",
1,
0,
NULL,
NULL,
val,
val[i] = (val[i] -
p0) * div_half_ro0_uref2;
(mesh_id,
"CP",
1,
0,
NULL,
NULL,
val,
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) {
cs_real_t div_half_ro0_uref2 = 1. / (0.5 * phys_pro->
ro0 * uref2);
char var_name[64];
int pref_rank;
xyz_ref,
&pref_id,
&pref_rank);
pref = pres[pref_id];
for (int col = 0; col < 5; col++) {
switch(col) {
case 0:
{
strncpy(var_name, "X/H", 64);
val[i] = face_cog[
f_id][0] / href;
}
}
break;
case 1:
{
strncpy(var_name, "CP", 64);
val[i] = (pres[c_id] - pref) * div_half_ro0_uref2;
}
}
break;
case 2:
{
strncpy(var_name, "CF", 64);
}
}
break;
case 3:
{
strncpy(var_name, "U/UREF", 64);
val[i] = copysign(val[i], stresses[i][0]);
}
}
break;
case 4:
{
strncpy(var_name, "YPLUS", 64);
}
}
break;
}
(mesh_id,
var_name,
1,
0,
NULL,
NULL,
val,
ts_post);
}
}
cs_lnum_t n_cells
Definition: cs_mesh.h:73
void const int * f_id
Definition: cs_gui.h:292
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
double precision, dimension(ncharm), save c2
Definition: cpincl.f90:233
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
#define CS_POST_MESH_VOLUME
Definition: cs_post.h:78
cs_fluid_properties_t * cs_get_glob_fluid_properties(void)
Definition: cs_physical_constants.c:524
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
cs_mesh_quantities_t * cs_glob_mesh_quantities
cs_real_t cs_real_3_t[3]
vector of 3 floating-point values
Definition: cs_defs.h:315
real(c_double), pointer, save ro0
reference density.
Definition: cstphy.f90:146
const cs_turb_model_t * cs_glob_turb_model
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(:), pointer distb
Definition: mesh.f90:188
cs_real_t * b_face_cog
Definition: cs_mesh_quantities.h:105
Definition: cs_field_pointer.h:74
#define CS_REAL_TYPE
Definition: cs_defs.h:407
cs_field_interpolate_t
Field interpolation modes.
Definition: cs_field_operator.h:54
Definition: cs_field_pointer.h:79
int itytur
Definition: cs_turbulence_model.h:99
const char * name
Definition: cs_field.h:126
int nt_cur
Definition: cs_time_step.h:61
double cs_real_t
Floating-point value.
Definition: cs_defs.h:302
cs_lnum_t * b_face_cells
Definition: cs_mesh.h:88
cs_lnum_2_t * i_face_cells
Definition: cs_mesh.h:87
#define CS_POST_WRITER_ALL_ASSOCIATED
Definition: cs_post.h:66
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
double uref
Definition: cs_turbulence_model.h:110
const cs_turb_ref_values_t * cs_glob_turb_ref_values
Definition: cs_mesh_quantities.h:90
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
Definition: cs_field_pointer.h:77
#define CS_POST_MESH_PROBES
Definition: cs_post.h:82
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
real(c_double), pointer, save uref
the characteristic flow velocity, used for the initialization of the turbulence. Negative value: not ...
Definition: cstphy.f90:619
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
const cs_turb_rans_model_t * cs_glob_turb_rans_model
cs_real_t * val
Definition: cs_field.h:145
cs_real_t * cell_cen
Definition: cs_mesh_quantities.h:92
Turbulence model general options descriptor.
Definition: cs_turbulence_model.h:75
#define BFT_MALLOC(_ptr, _ni, _type)
Allocate memory for _ni elements of type _type.
Definition: bft_mem.h:62
RANS turbulence model descriptor.
Definition: cs_turbulence_model.h:117
time step descriptor
Definition: cs_time_step.h:51
#define BFT_FREE(_ptr)
Free allocated memory.
Definition: bft_mem.h:101
#define CS_F_(e)
Macro used to return a field pointer by its enumerated value.
Definition: cs_field_pointer.h:51
Definition: cs_field_operator.h:56
Definition: cs_field_pointer.h:78
cs_real_t cs_real_6_t[6]
vector of 6 floating-point values
Definition: cs_defs.h:317
Definition: cs_field_pointer.h:75
double viscl0
Definition: cs_physical_constants.h:73
void cs_int_t cs_int_t cs_int_t cs_real_t * ts
Definition: cs_at_plugin.h:63
int cs_lnum_t
local mesh entity id
Definition: cs_defs.h:298
int cs_glob_rank_id
Definition: cs_defs.c:176
Definition: cs_field_pointer.h:76
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
double ro0
Definition: cs_physical_constants.h:72
void const cs_int_t *const const cs_int_t *const const cs_int_t *const const cs_int_t *const const cs_int_t *const const cs_int_t *const const cs_int_t *const const cs_int_t *const const cs_real_t *const const cs_real_t *const const cs_real_t const cs_real_t const cs_real_3_t vel[]
Definition: cs_divergence.h:64
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
void cs_mesh_sync_var_scal(cs_real_t *var)
Definition: cs_mesh.c:3214
Definition: cs_field_pointer.h:73
Fluid properties descriptor.
Definition: cs_physical_constants.h:61
int irijco
Definition: cs_turbulence_model.h:155
double precision, dimension(:,:), allocatable xpos
Positions.
Definition: atimbr.f90:103
void const cs_real_t * p0
Definition: cs_ctwr_air_props.h:85
double p0
Definition: cs_physical_constants.h:74
Field descriptor.
Definition: cs_field.h:124
cs_real_t * b_dist
Definition: cs_mesh_quantities.h:124
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
Definition: cs_field_pointer.h:67
double precision, dimension(ncharm), save c1
Definition: cpincl.f90:233