1 #ifndef __CS_TURBOMACHINERY_H__ 2 #define __CS_TURBOMACHINERY_H__ 92 double rotation_velocity,
93 const double rotation_axis[3],
94 const double rotation_invariant[3]);
cs_turbomachinery_model_t
Definition: cs_turbomachinery.h:50
Definition: cs_turbomachinery.h:54
void cs_turbomachinery_rotation_matrix(int rotor_num, double theta, cs_real_t matrix[3][4])
Compute rotation matrix.
Definition: cs_turbomachinery.c:1287
void cs_turbomachinery_set_model(cs_turbomachinery_model_t model)
Define rotor/stator model.
Definition: cs_turbomachinery.c:948
void cs_turbomachinery_relative_velocity(int rotor_num, const cs_real_t coords[3], cs_real_t velocity[3])
Compute velocity relative to fixed coordinates at a given point.
Definition: cs_turbomachinery.c:1433
void cs_turbomachinery_rotate_fields(const cs_real_t dt[])
Rotation of vector and tensor fields.
Definition: cs_turbomachinery.c:1338
Definition: cs_turbomachinery.h:53
#define BEGIN_C_DECLS
Definition: cs_defs.h:448
void cs_turbomachinery_initialize(void)
Initializations for turbomachinery computation.
Definition: cs_turbomachinery.c:1103
int cs_turbomachinery_join_add(const char *sel_criteria, float fraction, float plane, int verbosity, int visualization)
Add a cs_join_t structure to the list of rotor/stator joinings.
Definition: cs_turbomachinery.c:1033
Definition: cs_turbomachinery.h:52
const int * cs_turbomachinery_get_cell_rotor_num(void)
Return cell rotor number.
Definition: cs_turbomachinery.c:1310
double cs_turbomachinery_get_rotation_velocity(int rotor_num)
Return rotation velocity.
Definition: cs_turbomachinery.c:1324
void cs_turbomachinery_update_mesh(double t_cur_mob, double *t_elapsed)
Update mesh for unsteady rotor/stator computation.
Definition: cs_turbomachinery.c:1070
double cs_real_t
Floating-point value.
Definition: cs_defs.h:296
void matrix(const int *iconvp, const int *idiffp, const int *ndircp, const int *isym, const cs_real_t *thetap, const int *imucpp, const cs_real_t coefbp[], const cs_real_t cofbfp[], const cs_real_t rovsdt[], const cs_real_t i_massflux[], const cs_real_t b_massflux[], const cs_real_t i_visc[], const cs_real_t b_visc[], const cs_real_t xcpp[], cs_real_t da[], cs_real_t xa[])
Definition: cs_matrix_building.c:111
cs_turbomachinery_model_t cs_turbomachinery_get_model(void)
Return rotor/stator model.
Definition: cs_turbomachinery.c:969
void cs_turbomachinery_resize_cell_fields(void)
Resize cell-based fields.
Definition: cs_turbomachinery.c:1231
void cs_turbomachinery_add_rotor(const char *cell_criteria, double rotation_velocity, const double rotation_axis[3], const double rotation_invariant[3])
Define a rotor by its axis and cell selection criteria.
Definition: cs_turbomachinery.c:989
Definition: cs_field_pointer.h:64
double precision, dimension(:,:,:), allocatable theta
Definition: atimbr.f90:123
void cs_turbomachinery_finalize(void)
Free turbomachinery structure.
Definition: cs_turbomachinery.c:1177
void cs_turbomachinery_reinit_i_face_fields(void)
Reinitialize interior face-based fields.
Definition: cs_turbomachinery.c:1208
#define END_C_DECLS
Definition: cs_defs.h:449
void cs_turbomachinery_restart_mesh(double t_cur_mob, double *t_elapsed)
Read mesh from checkpoint for unsteady rotor/stator computation.
Definition: cs_turbomachinery.c:1086