Compressible examples

Local variables to be added

  /* Initialization */
 
  const cs_lnum_t n_b_faces = domain->mesh->n_b_faces;
  const cs_lnum_t *b_face_cells = domain->mesh->b_face_cells;
  const cs_real_3_t *restrict b_face_normal
    = (const cs_real_3_t *restrict)domain->mesh_quantities->b_face_normal;
 
  const cs_zone_t  *zn = NULL;
  const int n_fields = cs_field_n_fields();
  const cs_real_t *cpro_rho = CS_F_(rho)->val;
  const int keysca = cs_field_key_id("scalar_id");
 
  const cs_real_t viscl0 = cs_glob_fluid_properties->viscl0;
 
  /*==========================================================================
   * Assign boundary conditions to boundary faces here
 
   * For each subset:
   * - use selection criteria to filter boundary faces of a given subset
   * - loop on faces from a subset
   *   - set the boundary condition for each face
   *==========================================================================*/
 
  /* Example of inlet/outlet for which everything is known
 
   * Without assuming the subsonic or supersonic nature of the inlet
   * the user wishes to impose all the characteristics of the flow,
   * a supersonic inlet is a particular case.
 
   * The turbulence and the user scalars take a zero flux if the
   * velocity is outward. ---*/
 
  zn = cs_boundary_zone_by_name("1 and X <= 1.0");
  for (cs_lnum_t ilelt = 0; ilelt < zn->n_elts; ilelt++) {
 
    const cs_lnum_t face_id = zn->elt_ids[ilelt];
    const cs_lnum_t c_id = b_face_cells[face_id];
 
    bc_type[face_id] = CS_ESICF;
 
    /* Velocity */
    CS_F_(vel)->bc_coeffs->rcodcl1[face_id] = 5.0;
    CS_F_(vel)->bc_coeffs->rcodcl1[n_b_faces*1 + face_id] = 0;
    CS_F_(vel)->bc_coeffs->rcodcl1[n_b_faces*2 + face_id] = 0;
 
    /* Pressure, Density, Temperature, Total Specific Energy
 
     *     Only 2 of the 4 variables are independant,
     *     hence one can impose values for any couple of variables
     *     (except Temperature-Energy) and the two other variables
     *     will be computed automatically */
 
    /* Choose a couple of variables which values are to be imposed
     * and delete the others (that will be computed with the help of
     * the thermodynamic laws in cs_cf_thermo.c). */
 
    /* Pressure (in Pa) */
    CS_F_(p)->bc_coeffs->rcodcl1[face_id] = 5.5;
 
    /* Temperature (in K) */
    CS_F_(t_kelvin)->bc_coeffs->rcodcl1[face_id] = 300.0;
 
    /* Specific Total Energy (in J/kg) */
    CS_F_(e_tot)->bc_coeffs->rcodcl1[face_id] = 355.e3;
 
    /* Turbulence */
 
    cs_real_t uref2 =  0;
    for(int ii = 0; ii < CS_F_(vel)->dim; ii++)
      uref2 += cs_math_pow2(CS_F_(vel)->bc_coeffs->rcodcl1[n_b_faces*ii +face_id]);
    cs_parall_sum(1, CS_REAL_TYPE, &uref2);
    uref2 = cs_math_fmax(uref2, 1.e-12);
 
    /* Turbulence example computed using equations valid for a pipe.
 
     * We will be careful to specify a hydraulic diameter adapted
     * to the current inlet.
 
     * We will also be careful if necessary to use a more precise
     * formula for the dynamic viscosity use in the calculation of
     * the Reynolds number (especially if it is variable, it may be
     * useful to take the law from 'cs_user_physical_properties'.
     * Here, we use by default the 'viscl0" value.
     * Regarding the density, we have access to its value at boundary
     * faces (romb) so this value is the one used here (specifically,
     * it is consistent with the processing in 'cs_user_physical_properties',
     * in case of variable density) */
 
    /* Hydraulic diameter */
    const cs_real_t dhy = 0.075;
 
    const cs_real_t rhomoy = cpro_rho[c_id];
 
    cs_turbulence_bc_inlet_hyd_diam(face_id,
                                    uref2,
                                    dhy,
                                    rhomoy,
                                    viscl0);
 
    /*  Handle scalars (avoid modifying rho and energy) */
    for (int f_id = 0; f_id < n_fields; f_id++) {
      cs_field_t *fld  = cs_field_by_id(f_id);
      if ((fld == CS_F_(rho)) || (fld == CS_F_(e_tot)))
        continue;
      int sc_id = -1;
      if (fld->type & CS_FIELD_VARIABLE)
        sc_id = cs_field_get_key_int(fld, keysca) - 1;
      if (sc_id < 0)
        continue;
      fld->bc_coeffs->rcodcl1[face_id] = 1.0;
    }
  }
  /* Supersonic outlet example
 
   * All the characteristics are outward,
   * nothing needs to be imposed (only internal values are used
   * to compute the boundary flux).
 
   * for the turbulence and the scalar, if values of rcodcl are
   * provided here, we impose them as Dirichlet if the mass flux is
   * inward ; otherwise a zero flux is imposed (outward mass flux or
   * rcodcl values given here).
   * Note that for turbulence, RCODCL has to be filled in for all
   * turbulent variable (otherwise a zero flux is imposed). */
 
   zn = cs_boundary_zone_by_name("2");
 
   for (cs_lnum_t ilelt = 0; ilelt < zn->n_elts; ilelt++) {
     const cs_lnum_t face_id = zn->elt_ids[ilelt];
     bc_type[face_id] = CS_SSPCF;
   }
   /* Example of subsonic inlet (total pressure, total enthalpy) */
 
   zn = cs_boundary_zone_by_name("3");
 
   for (cs_lnum_t ilelt = 0; ilelt < zn->n_elts; ilelt++) {
 
     const cs_lnum_t face_id = zn->elt_ids[ilelt];
 
     bc_type[face_id] = CS_EPHCF;
 
     /* Total pressure (in Pa) */
     CS_F_(p)->bc_coeffs->rcodcl1[face_id] = 1e5;
 
     /* Total energy */
     CS_F_(e_tot)->bc_coeffs->rcodcl1[face_id] = 294465.0;
 
     /* Direction of the velocity: normal to inlet faces */
     for(int ii = 0; ii < CS_F_(vel)->dim; ii++)
       CS_F_(vel)->bc_coeffs->rcodcl1[n_b_faces*ii +face_id]
         = -b_face_normal[face_id][ii];
 
     /* Turbulence (no turbulence)*/
 
     /*  Handle scalars
         (do not loop on nscal to avoid modifying rho and energy) */
     for (int f_id = 0; f_id < n_fields; f_id++) {
       cs_field_t *fld  = cs_field_by_id(f_id);
       if ((fld == CS_F_(rho)) || (fld == CS_F_(e_tot)))
         continue;
       int sc_id = -1;
       if (fld->type & CS_FIELD_VARIABLE)
         sc_id = cs_field_get_key_int(fld, keysca) - 1;
       if (sc_id < 0)
         continue;
       fld->bc_coeffs->rcodcl1[face_id] = 1.0;
     }
 
   }
   /* Subsonic outlet example */
 
   zn = cs_boundary_zone_by_name("4");
 
   for (cs_lnum_t ilelt = 0; ilelt < zn->n_elts; ilelt++) {
     const cs_lnum_t face_id = zn->elt_ids[ilelt];
     bc_type[face_id] = CS_SOPCF;
 
     /* Pressure (in Pa) */
     CS_F_(p)->bc_coeffs->rcodcl1[face_id] = 5.e5;
   }
   /* Wall example */
 
   zn = cs_boundary_zone_by_name("5");
 
   for (cs_lnum_t ilelt = 0; ilelt < zn->n_elts; ilelt++) {
     const cs_lnum_t face_id = zn->elt_ids[ilelt];
     bc_type[face_id] = CS_SMOOTHWALL;
 
     /* Sliding wall */
 
     /* By default, the wall does not slide.
      * If the wall slides, define the nonzero components of its velocity.
      * The velocity will be projected in a plane tangent to the wall.
      * In the following example, we prescribe Ux = 1. */
 
     CS_F_(vel)->bc_coeffs->rcodcl1[face_id] = 1.0;
 
     /* Prescribed temperature
      *
      * By default, the wall is adiabatic.
      * If the wall has a prescribed temperature, indicate it by setting
      * icodcl = 5 and define a value in Kelvin in rcodcl1
      * In the following example, we prescribe T = 293.15 K
      * (example activated if needed=1) */
 
     CS_F_(t_kelvin)->bc_coeffs->icodcl[face_id] = 5;
     CS_F_(t_kelvin)->bc_coeffs->rcodcl1[face_id] = 20. + 273.15;
 
     /* Prescribed flux
 
      * By default, the wall is adiabatic.
      * If the wall has a prescribed flux, indicate it by setting
      * icodcl = 3 and define the value in Watt/m2 in rcodcl3
      * In the following example, we prescribe a flux of 1000 W/m2
      * - a midday in the summer - (example is activated if needed=1) */
 
     CS_F_(t_kelvin)->bc_coeffs->icodcl[face_id] = 3;
     CS_F_(t_kelvin)->bc_coeffs->rcodcl3[face_id] = 1000.0;
   }

Initialization and finalization

Initialization and finalization is similar to that of the base examples

Example 1

Example of input / output for which everything is known.

Without presuming subsonic or supersonic character, the user wishes to impose all the flow characteristics. A supersonic inlet is a special case.

If the speed is outgoing, an homogenous Neumann is imposed on turbulence and user scalars.

 
  zn = cs_boundary_zone_by_name("1 and X <= 1.0");
  for (cs_lnum_t ilelt = 0; ilelt < zn->n_elts; ilelt++) {
 
    const cs_lnum_t face_id = zn->elt_ids[ilelt];
    const cs_lnum_t c_id = b_face_cells[face_id];
 
    bc_type[face_id] = CS_ESICF;
 
    /* Velocity */
    CS_F_(vel)->bc_coeffs->rcodcl1[face_id] = 5.0;
    CS_F_(vel)->bc_coeffs->rcodcl1[n_b_faces*1 + face_id] = 0;
    CS_F_(vel)->bc_coeffs->rcodcl1[n_b_faces*2 + face_id] = 0;
 
    /* Pressure, Density, Temperature, Total Specific Energy
 
     *     Only 2 of the 4 variables are independant,
     *     hence one can impose values for any couple of variables
     *     (except Temperature-Energy) and the two other variables
     *     will be computed automatically */
 
    /* Choose a couple of variables which values are to be imposed
     * and delete the others (that will be computed with the help of
     * the thermodynamic laws in cs_cf_thermo.c). */
 
    /* Pressure (in Pa) */
    CS_F_(p)->bc_coeffs->rcodcl1[face_id] = 5.5;
 
    /* Temperature (in K) */
    CS_F_(t_kelvin)->bc_coeffs->rcodcl1[face_id] = 300.0;
 
    /* Specific Total Energy (in J/kg) */
    CS_F_(e_tot)->bc_coeffs->rcodcl1[face_id] = 355.e3;
 
    /* Turbulence */
 
    cs_real_t uref2 =  0;
    for(int ii = 0; ii < CS_F_(vel)->dim; ii++)
      uref2 += cs_math_pow2(CS_F_(vel)->bc_coeffs->rcodcl1[n_b_faces*ii +face_id]);
    cs_parall_sum(1, CS_REAL_TYPE, &uref2);
    uref2 = cs_math_fmax(uref2, 1.e-12);
 
    /* Turbulence example computed using equations valid for a pipe.
 
     * We will be careful to specify a hydraulic diameter adapted
     * to the current inlet.
 
     * We will also be careful if necessary to use a more precise
     * formula for the dynamic viscosity use in the calculation of
     * the Reynolds number (especially if it is variable, it may be
     * useful to take the law from 'cs_user_physical_properties'.
     * Here, we use by default the 'viscl0" value.
     * Regarding the density, we have access to its value at boundary
     * faces (romb) so this value is the one used here (specifically,
     * it is consistent with the processing in 'cs_user_physical_properties',
     * in case of variable density) */
 
    /* Hydraulic diameter */
    const cs_real_t dhy = 0.075;
 
    const cs_real_t rhomoy = cpro_rho[c_id];
 
    cs_turbulence_bc_inlet_hyd_diam(face_id,
                                    uref2,
                                    dhy,
                                    rhomoy,
                                    viscl0);
 
    /*  Handle scalars (avoid modifying rho and energy) */
    for (int f_id = 0; f_id < n_fields; f_id++) {
      cs_field_t *fld  = cs_field_by_id(f_id);
      if ((fld == CS_F_(rho)) || (fld == CS_F_(e_tot)))
        continue;
      int sc_id = -1;
      if (fld->type & CS_FIELD_VARIABLE)
        sc_id = cs_field_get_key_int(fld, keysca) - 1;
      if (sc_id < 0)
        continue;
      fld->bc_coeffs->rcodcl1[face_id] = 1.0;
    }
  }

Example 2

Example supersonic output

All features are output. Internal values are used to calculate the flow edge, they should not be imposed.

For turbulence and scalar, if RCODCL values are provided, they will be used in Dirichlet if the mass flow is incoming, otherwise a null flow is imposed (flow outgoing mass or RCODCL informed here). Note that for turbulence RCODCL must be defined for all turbulent variables. Otherwise a null flow is applied).

Example of supersonic outlet

All characteristics exit. Nothing should be prescribed (the internal values are used to the computation of boundary fluxes).

For turbulence and scalars, if we provide here values ofrcodcl, we prescribe them as Dirichlet values if the mass flux is entering. otherwise, we prescribe a zero flux (outgoing mass flux or rcodcl defined here). Note that for turbulence, rcodcl should be set for all turbulent variables (otherwise, we apply a zero flux).

   zn = cs_boundary_zone_by_name("2");
 
   for (cs_lnum_t ilelt = 0; ilelt < zn->n_elts; ilelt++) {
     const cs_lnum_t face_id = zn->elt_ids[ilelt];
     bc_type[face_id] = CS_SSPCF;
   }

Example 3

Subsonic input example with density and velocity.

Two of three characteristics are incoming: two informations must be provided, third is deduced by a scenario of 2-contact and 3-relaxation in the field. Here we choose to give (rho, U).

Example of a subsonic inlet (density, velocity)

2 characteristcs out ot 3 enter: both informations should be provided the third is deducted by a scenario of 2-contact and 3-relaxation in the domain. Here, whe choose to give (rho, U).

   zn = cs_boundary_zone_by_name("3");
 
   for (cs_lnum_t ilelt = 0; ilelt < zn->n_elts; ilelt++) {
 
     const cs_lnum_t face_id = zn->elt_ids[ilelt];
 
     bc_type[face_id] = CS_EPHCF;
 
     /* Total pressure (in Pa) */
     CS_F_(p)->bc_coeffs->rcodcl1[face_id] = 1e5;
 
     /* Total energy */
     CS_F_(e_tot)->bc_coeffs->rcodcl1[face_id] = 294465.0;
 
     /* Direction of the velocity: normal to inlet faces */
     for(int ii = 0; ii < CS_F_(vel)->dim; ii++)
       CS_F_(vel)->bc_coeffs->rcodcl1[n_b_faces*ii +face_id]
         = -b_face_normal[face_id][ii];
 
     /* Turbulence (no turbulence)*/
 
     /*  Handle scalars
         (do not loop on nscal to avoid modifying rho and energy) */
     for (int f_id = 0; f_id < n_fields; f_id++) {
       cs_field_t *fld  = cs_field_by_id(f_id);
       if ((fld == CS_F_(rho)) || (fld == CS_F_(e_tot)))
         continue;
       int sc_id = -1;
       if (fld->type & CS_FIELD_VARIABLE)
         sc_id = cs_field_get_key_int(fld, keysca) - 1;
       if (sc_id < 0)
         continue;
       fld->bc_coeffs->rcodcl1[face_id] = 1.0;
     }
 
   }

Example 4

Subsonic outlet example

1 characteristic out of 3 exits: 1 information must be given the 2 others are deduced by a 2-contact and 3-relaxation in the domain. Here we choose to definer P.

Turbulence and user scalars take a zero flux.

   zn = cs_boundary_zone_by_name("4");
 
   for (cs_lnum_t ilelt = 0; ilelt < zn->n_elts; ilelt++) {
     const cs_lnum_t face_id = zn->elt_ids[ilelt];
     bc_type[face_id] = CS_SOPCF;
 
     /* Pressure (in Pa) */
     CS_F_(p)->bc_coeffs->rcodcl1[face_id] = 5.e5;
   }

Example 5

Wall example

   zn = cs_boundary_zone_by_name("5");
 
   for (cs_lnum_t ilelt = 0; ilelt < zn->n_elts; ilelt++) {
     const cs_lnum_t face_id = zn->elt_ids[ilelt];
     bc_type[face_id] = CS_SMOOTHWALL;
 
     /* Sliding wall */
 
     /* By default, the wall does not slide.
      * If the wall slides, define the nonzero components of its velocity.
      * The velocity will be projected in a plane tangent to the wall.
      * In the following example, we prescribe Ux = 1. */
 
     CS_F_(vel)->bc_coeffs->rcodcl1[face_id] = 1.0;
 
     /* Prescribed temperature
      *
      * By default, the wall is adiabatic.
      * If the wall has a prescribed temperature, indicate it by setting
      * icodcl = 5 and define a value in Kelvin in rcodcl1
      * In the following example, we prescribe T = 293.15 K
      * (example activated if needed=1) */
 
     CS_F_(t_kelvin)->bc_coeffs->icodcl[face_id] = 5;
     CS_F_(t_kelvin)->bc_coeffs->rcodcl1[face_id] = 20. + 273.15;
 
     /* Prescribed flux
 
      * By default, the wall is adiabatic.
      * If the wall has a prescribed flux, indicate it by setting
      * icodcl = 3 and define the value in Watt/m2 in rcodcl3
      * In the following example, we prescribe a flux of 1000 W/m2
      * - a midday in the summer - (example is activated if needed=1) */
 
     CS_F_(t_kelvin)->bc_coeffs->icodcl[face_id] = 3;
     CS_F_(t_kelvin)->bc_coeffs->rcodcl3[face_id] = 1000.0;
   }