CSourcePieceWise_TurbSA Class Reference

Class for integrating the source terms of the Spalart-Allmaras turbulence model equation. More...

#include <numerics_structure.hpp>

Inheritance diagram for CSourcePieceWise_TurbSA:

Public Member Functions
	CSourcePieceWise_TurbSA (unsigned short val_nDim, unsigned short val_nVar, CConfig *config)
	Constructor of the class. More...
	~CSourcePieceWise_TurbSA (void)
	Destructor of the class.
void	ComputeResidual (su2double *val_residual, su2double **val_Jacobian_i, su2double **val_Jacobian_j, CConfig *config)
	Residual for source term integration. More...
void	SetIntermittency (su2double intermittency_in)
	Residual for source term integration. More...
void	SetProduction (su2double val_production)
	Residual for source term integration. More...
void	SetDestruction (su2double val_destruction)
	Residual for source term integration. More...
void	SetCrossProduction (su2double val_crossproduction)
	Residual for source term integration. More...
su2double	GetProduction (void)
	______________.
su2double	GetDestruction (void)
	______________.
su2double	GetCrossProduction (void)
	______________.
Public Member Functions inherited from CNumerics
	CNumerics (void)
	Constructor of the class.
	CNumerics (unsigned short val_nDim, unsigned short val_nVar, CConfig *config)
virtual	~CNumerics (void)
	Destructor of the class.
su2double	Determinant_3x3 (su2double A00, su2double A01, su2double A02, su2double A10, su2double A11, su2double A12, su2double A20, su2double A21, su2double A22)
	Compute the determinant of a 3 by 3 matrix. More...
void	SetPastSol (su2double *val_u_nM1, su2double *val_u_n, su2double *val_u_nP1)
	Set the solution at different times. More...
void	SetPastVolume (su2double val_volume_nM1, su2double val_volume_n, su2double val_volume_nP1)
	Set the control volume at different times. More...
void	SetTimeStep (su2double val_timestep)
	Set the time step. More...
virtual su2double	GetPrecond_Beta ()
	Get the Preconditioning Beta. More...
void	SetVelocity2_Inf (su2double val_velocity2)
	Set the freestream velocity square. More...
void	SetVorticity (su2double *val_vorticity_i, su2double *val_vorticity_j)
	Set the value of the vorticity. More...
void	SetStrainMag (su2double val_strainmag_i, su2double val_strainmag_j)
	Set the value of the rate of strain magnitude. More...
void	SetConservative (su2double *val_u_i, su2double *val_u_j)
	Set the value of the conservative variables. More...
void	SetConservative_ZeroOrder (su2double *val_u_i, su2double *val_u_j)
	Set the value of the conservative variables withour reconstruction. More...
void	SetPrimitive (su2double *val_v_i, su2double *val_v_j)
	Set the value of the primitive variables. More...
void	SetSecondary (su2double *val_s_i, su2double *val_s_j)
	Set the value of the primitive variables. More...
void	SetConservative (su2double *val_u_0, su2double *val_u_1, su2double *val_u_2)
	Set the value of the conservative variables. More...
void	SetConservative (su2double *val_u_0, su2double *val_u_1, su2double *val_u_2, su2double *val_u_3)
	Set the value of the conservative variables. More...
void	SetConsVarGradient (su2double **val_consvar_grad_i, su2double **val_consvar_grad_j)
	Set the gradient of the conservative variables. More...
void	SetConsVarGradient (su2double **val_consvar_grad_0, su2double **val_consvar_grad_1, su2double **val_consvar_grad_2)
	Set the gradient of the conservative variables. More...
void	SetConsVarGradient (su2double **val_consvar_grad_0, su2double **val_consvar_grad_1, su2double **val_consvar_grad_2, su2double **val_consvar_grad_3)
	Set the gradient of the conservative variables. More...
void	SetConsVarGradient (su2double **val_consvar_grad)
	Set the gradient of the conservative variables. More...
void	SetPrimVarGradient (su2double **val_primvar_grad_i, su2double **val_primvar_grad_j)
	Set the gradient of the primitive variables. More...
void	SetPrimVarLimiter (su2double *val_primvar_lim_i, su2double *val_primvar_lim_j)
	Set the Limiter of the primitive variables. More...
void	SetAdjointVar (su2double *val_psi_i, su2double *val_psi_j)
	Set the value of the adjoint variable. More...
void	SetAdjointVarGradient (su2double **val_psivar_grad_i, su2double **val_psivar_grad_j)
	Set the gradient of the adjoint variables. More...
void	SetAdjointVarLimiter (su2double *val_psivar_lim_i, su2double *val_psivar_lim_j)
	Set the limiter of the adjoint variables. More...
void	SetTurbVar (su2double *val_turbvar_i, su2double *val_turbvar_j)
	Set the value of the turbulent variable. More...
void	SetTransVar (su2double *val_transvar_i, su2double *val_transvar_j)
	Set the value of the turbulent variable. More...
void	SetTurbVarGradient (su2double **val_turbvar_grad_i, su2double **val_turbvar_grad_j)
	Set the gradient of the turbulent variables. More...
void	SetTransVarGradient (su2double **val_transvar_grad_i, su2double **val_transvar_grad_j)
	Set the gradient of the turbulent variables. More...
void	SetTurbAdjointVar (su2double *val_turbpsivar_i, su2double *val_turbpsivar_j)
	Set the value of the adjoint turbulent variable. More...
void	SetTurbAdjointGradient (su2double **val_turbpsivar_grad_i, su2double **val_turbpsivar_grad_j)
	Set the gradient of the adjoint turbulent variables. More...
virtual void	SetF1blending (su2double val_F1_i, su2double val_F1_j)
	Set the value of the first blending function. More...
virtual void	SetF2blending (su2double val_F1_i, su2double val_F1_j)
	Set the value of the second blending function. More...
virtual void	SetCrossDiff (su2double val_CDkw_i, su2double val_CDkw_j)
	Set the value of the cross diffusion for the SST model. More...
void	SetAuxVarGrad (su2double *val_auxvargrad_i, su2double *val_auxvargrad_j)
	Set the gradient of the auxiliary variables. More...
void	SetDiffusionCoeff (su2double *val_diffusioncoeff_i, su2double *val_diffusioncoeff_j)
	Set the diffusion coefficient. More...
void	SetLaminarViscosity (su2double val_laminar_viscosity_i, su2double val_laminar_viscosity_j)
	Set the laminar viscosity. More...
void	SetThermalConductivity (su2double val_thermal_conductivity_i, su2double val_thermal_conductivity_j)
	Set the thermal conductivity (translational/rotational) More...
void	SetThermalConductivity_ve (su2double val_thermal_conductivity_ve_i, su2double val_thermal_conductivity_ve_j)
	Set the thermal conductivity (translational/rotational) More...
void	SetEddyViscosity (su2double val_eddy_viscosity_i, su2double val_eddy_viscosity_j)
	Set the eddy viscosity. More...
void	SetTurbKineticEnergy (su2double val_turb_ke_i, su2double val_turb_ke_j)
	Set the turbulent kinetic energy. More...
void	SetDistance (su2double val_dist_i, su2double val_dist_j)
	Set the value of the distance from the nearest wall. More...
void	SetCoord (su2double *val_coord_i, su2double *val_coord_j)
	Set coordinates of the points. More...
void	SetCoord (su2double *val_coord_0, su2double *val_coord_1, su2double *val_coord_2)
void	SetCoord (su2double *val_coord_0, su2double *val_coord_1, su2double *val_coord_2, su2double *val_coord_3)
void	SetGridVel (su2double *val_gridvel_i, su2double *val_gridvel_j)
	Set the velocity of the computational grid. More...
void	SetWindGust (su2double *val_windgust_i, su2double *val_windgust_j)
	Set the wind gust value. More...
void	SetWindGustDer (su2double *val_windgustder_i, su2double *val_windgustder_j)
	Set the wind gust derivatives values. More...
void	SetPressure (su2double val_pressure_i, su2double val_pressure_j)
	Set the value of the pressure. More...
void	SetDensity (su2double val_densityinc_i, su2double val_densityinc_j)
	Set the value of the density for the incompressible solver. More...
void	SetBetaInc2 (su2double val_betainc2_i, su2double val_betainc2_j)
	Set the value of the beta for incompressible flows. More...
void	SetSoundSpeed (su2double val_soundspeed_i, su2double val_soundspeed_j)
	Set the value of the sound speed. More...
void	SetTemperature (su2double val_temp_i, su2double val_temp_j)
	Set the value of the temperature. More...
void	SetEnthalpy (su2double val_enthalpy_i, su2double val_enthalpy_j)
	Set the value of the enthalpy. More...
void	SetLambda (su2double val_lambda_i, su2double val_lambda_j)
	Set the value of the spectral radius. More...
void	SetUndivided_Laplacian (su2double *val_und_lapl_i, su2double *val_und_lapl_j)
	Set the value of undivided laplacian. More...
void	SetSensor (su2double val_sensor_i, su2double val_sensor_j)
	Set the value of the pressure sensor. More...
void	SetNeighbor (unsigned short val_neighbor_i, unsigned short val_neighbor_j)
	Set the number of neighbor to a point. More...
void	SetNormal (su2double *val_normal)
	Set the value of the normal vector to the face between two points. More...
void	SetVolume (su2double val_volume)
	Set the value of the volume of the control volume. More...
void	SetRhosIndex (unsigned short val_Index)
	Retrieves the value of the species density in the primitive variable vector. More...
void	SetRhoIndex (unsigned short val_Index)
	Retrieves the value of the species density in the primitive variable vector. More...
void	SetPIndex (unsigned short val_Index)
	Retrieves the value of the species density in the primitive variable vector. More...
void	SetTIndex (unsigned short val_Index)
	Retrieves the value of the species density in the primitive variable vector. More...
void	SetTveIndex (unsigned short val_Index)
	Retrieves the value of the species density in the primitive variable vector. More...
void	SetVelIndex (unsigned short val_Index)
	Retrieves the value of the velocity index in the primitive variable vector. More...
void	SetHIndex (unsigned short val_Index)
	Retrieves the value of the species density in the primitive variable vector. More...
void	SetAIndex (unsigned short val_Index)
	Retrieves the value of the species density in the primitive variable vector. More...
void	SetRhoCvtrIndex (unsigned short val_Index)
	Retrieves the value of the species density in the primitive variable vector. More...
void	SetRhoCvveIndex (unsigned short val_Index)
	Retrieves the value of the species density in the primitive variable vector. More...
void	SetdPdU (su2double *val_dPdU_i, su2double *val_dPdU_j)
	Sets the value of the derivative of pressure w.r.t. species density. More...
void	SetdTdU (su2double *val_dTdU_i, su2double *val_dTdU_j)
	Sets the value of the derivative of temperature w.r.t. species density. More...
void	SetdTvedU (su2double *val_dTvedU_i, su2double *val_dTvedU_j)
	Sets the value of the derivative of vib-el. temperature w.r.t. species density. More...
void	GetInviscidFlux (su2double val_density, su2double *val_velocity, su2double val_pressure, su2double val_enthalpy)
	Get the inviscid fluxes. More...
void	GetViscousFlux (su2double *val_primvar, su2double **val_gradprimvar, su2double val_laminar_viscosity, su2double val_eddy_viscosity, su2double val_mach_inf)
	Get the viscous fluxes. More...
void	GetInviscidProjFlux (su2double *val_density, su2double *val_velocity, su2double *val_pressure, su2double *val_enthalpy, su2double *val_normal, su2double *val_Proj_Flux)
	Compute the projected inviscid flux vector. More...
void	GetInviscidArtCompProjFlux (su2double *val_density, su2double *val_velocity, su2double *val_pressure, su2double *val_betainc2, su2double *val_normal, su2double *val_Proj_Flux)
	Compute the projected inviscid flux vector for incompresible simulations. More...
void	GetViscousProjFlux (su2double *val_primvar, su2double **val_gradprimvar, su2double val_turb_ke, su2double *val_normal, su2double val_laminar_viscosity, su2double val_eddy_viscosity)
	Compute the projection of the viscous fluxes into a direction. More...
void	GetViscousProjFlux (su2double *val_primvar, su2double **val_gradprimvar, su2double val_turb_ke, su2double *val_normal, su2double val_laminar_viscosity, su2double val_eddy_viscosity, su2double val_thermal_conductivity, su2double val_heat_capacity_cp)
	Compute the projection of the viscous fluxes into a direction for general fluid model. More...
void	GetViscousArtCompProjFlux (su2double **val_gradprimvar, su2double *val_normal, su2double val_laminar_viscosity, su2double val_eddy_viscosity)
void	GetInviscidProjJac (su2double *val_velocity, su2double *val_energy, su2double *val_normal, su2double val_scale, su2double **val_Proj_Jac_tensor)
	Compute the projection of the inviscid Jacobian matrices. More...
void	GetInviscidArtCompProjJac (su2double *val_density, su2double *val_velocity, su2double *val_betainc2, su2double *val_normal, su2double val_scale, su2double **val_Proj_Jac_tensor)
	Compute the projection of the inviscid Jacobian matrices (artificial compresibility). More...
void	GetInviscidProjJac (su2double *val_velocity, su2double *val_enthalphy, su2double *val_chi, su2double *val_kappa, su2double *val_normal, su2double val_scale, su2double **val_Proj_Jac_tensor)
	Compute the projection of the inviscid Jacobian matrices for general fluid model. More...
void	GetViscousProjJacs (su2double *val_Mean_PrimVar, su2double val_laminar_viscosity, su2double val_eddy_viscosity, su2double val_dist_ij, su2double *val_normal, su2double val_dS, su2double *val_Proj_Visc_Flux, su2double **val_Proj_Jac_Tensor_i, su2double **val_Proj_Jac_Tensor_j)
	TSL-Approximation of Viscous NS Jacobians. More...
void	GetViscousProjJacs (su2double *val_Mean_PrimVar, su2double **val_gradprimvar, su2double *val_Mean_SecVar, su2double val_laminar_viscosity, su2double val_eddy_viscosity, su2double val_thermal_conductivity, su2double val_heat_capacity_cp, su2double val_dist_ij, su2double *val_normal, su2double val_dS, su2double *val_Proj_Visc_Flux, su2double **val_Proj_Jac_Tensor_i, su2double **val_Proj_Jac_Tensor_j)
	TSL-Approximation of Viscous NS Jacobians for arbitrary equations of state. More...
void	GetPrimitive2Conservative (su2double *val_Mean_PrimVar, su2double *val_Mean_SecVar, su2double **val_Jac_PC)
	Mapping between primitives variables P and conservatives variables C. More...
void	GetViscousArtCompProjJacs (su2double val_laminar_viscosity, su2double val_eddy_viscosity, su2double val_dist_ij, su2double *val_normal, su2double val_dS, su2double **val_Proj_Jac_Tensor_i, su2double **val_Proj_Jac_Tensor_j)
	Compute the projection of the viscous Jacobian matrices. More...
void	GetPMatrix (su2double *val_density, su2double *val_velocity, su2double *val_soundspeed, su2double *val_enthalpy, su2double *val_chi, su2double *val_kappa, su2double *val_normal, su2double **val_p_tensor)
	Computation of the matrix P for a generic fluid model. More...
void	GetPMatrix (su2double *val_density, su2double *val_velocity, su2double *val_soundspeed, su2double *val_normal, su2double **val_p_tensor)
	Computation of the matrix P, this matrix diagonalize the conservative Jacobians in the form $P^{-1}(A.Normal)P=Lambda$. More...
void	GetinvRinvPe (su2double Beta2, su2double val_enthalpy, su2double val_soundspeed, su2double val_density, su2double *val_velocity, su2double **val_invR_invPe)
	Computation of the matrix Rinv*Pe. More...
void	GetRMatrix (su2double val_pressure, su2double val_soundspeed, su2double val_density, su2double *val_velocity, su2double **val_invR_invPe)
	Computation of the matrix R. More...
void	GetRMatrix (su2double val_soundspeed, su2double val_density, su2double *val_normal, su2double **R_Matrix)
	Computation of the matrix R. More...
void	GetLMatrix (su2double val_soundspeed, su2double val_density, su2double *val_normal, su2double **L_Matrix)
	Computation of the matrix R. More...
void	GetPrecondJacobian (su2double Beta2, su2double r_hat, su2double s_hat, su2double t_hat, su2double rB2a2, su2double *val_Lambda, su2double *val_normal, su2double **val_absPeJac)
	Computation of the matrix Td, this matrix diagonalize the preconditioned conservative Jacobians in the form $Tg |Lambda| Td = Pc{-1}|Pc (A.Normal)|$. More...
void	GetPArtCompMatrix (su2double *val_density, su2double *val_velocity, su2double *val_betainv2, su2double *val_normal, su2double **val_p_tensor)
	Computation of the matrix P (artificial compresibility), this matrix diagonalize the conservative Jacobians in the form $P^{-1}(A.Normal)P=Lambda$. More...
void	GetPMatrix_inv (su2double **val_invp_tensor, su2double *val_density, su2double *val_velocity, su2double *val_soundspeed, su2double *val_chi, su2double *val_kappa, su2double *val_normal)
	Computation of the matrix P^{-1}, this matrix diagonalize the conservative Jacobians in the form $P^{-1}(A.Normal)P=Lambda$. More...
void	GetPMatrix_inv (su2double *val_density, su2double *val_velocity, su2double *val_soundspeed, su2double *val_normal, su2double **val_invp_tensor)
	Computation of the matrix P^{-1}, this matrix diagonalize the conservative Jacobians in the form $P^{-1}(A.Normal)P=Lambda$. More...
void	GetPArtCompMatrix_inv (su2double *val_density, su2double *val_velocity, su2double *val_betainv2, su2double *val_normal, su2double **val_invp_tensor)
	Computation of the matrix P^{-1} (artificial compresibility), this matrix diagonalize the conservative Jacobians in the form $P^{-1}(A.Normal)P=Lambda$. More...
void	GetAdjViscousFlux_Jac (su2double Pressure_i, su2double Pressure_j, su2double Density_i, su2double Density_j, su2double ViscDens_i, su2double ViscDens_j, su2double *Velocity_i, su2double *Velocity_j, su2double sq_vel_i, su2double sq_vel_j, su2double XiDens_i, su2double XiDens_j, su2double **Mean_GradPhi, su2double *Mean_GradPsiE, su2double dPhiE_dn, su2double *Normal, su2double *Edge_Vector, su2double dist_ij_2, su2double *val_residual_i, su2double *val_residual_j, su2double **val_Jacobian_ii, su2double **val_Jacobian_ij, su2double **val_Jacobian_ji, su2double **val_Jacobian_jj, bool implicit)
	Compute viscous residual and jacobian.
void	GetJacInviscidLambda_fabs (su2double *val_velocity, su2double val_soundspeed, su2double *val_normal, su2double *val_Lambda_Vector)
	Computation of the projected inviscid lambda (eingenvalues). More...
virtual void	ComputeResidual (su2double *val_residual, CConfig *config)
	Compute the numerical residual. More...
virtual void	ComputeResidual (su2double *val_residual_i, su2double *val_residual_j)
virtual void	ComputeResidual_TransLM (su2double *val_residual, su2double **val_Jacobian_i, su2double **val_Jacobian_j, CConfig *config, su2double &gamma_sep)
virtual void	ComputeResidual (su2double *val_residual_i, su2double *val_residual_j, CConfig *config)
virtual void	ComputeResidual (su2double *val_residual, su2double **val_Jacobian_i, su2double **val_Jacobian_j, su2double **val_JacobianMeanFlow_i, su2double **val_JacobianMeanFlow_j, CConfig *config)
virtual void	ComputeResidual (su2double **val_Jacobian_i, su2double **val_Jacobian_j, CConfig *config)
virtual void	ComputeResidual (su2double *val_resconv, su2double *val_resvisc, su2double **val_Jacobian_i, su2double **val_Jacobian_j, CConfig *config)
virtual void	ComputeResidual (su2double *val_residual_i, su2double *val_residual_j, su2double **val_Jacobian_ii, su2double **val_Jacobian_ij, su2double **val_Jacobian_ji, su2double **val_Jacobian_jj, CConfig *config)
virtual void	ComputeResidual (su2double *val_resconv_i, su2double *val_resvisc_i, su2double *val_resconv_j, su2double *val_resvisc_j, su2double **val_Jacobian_ii, su2double **val_Jacobian_ij, su2double **val_Jacobian_ji, su2double **val_Jacobian_jj, CConfig *config)
virtual void	ComputeResidual (su2double **val_stiffmatrix_elem, CConfig *config)
virtual void	ComputeResidual (su2double *val_residual, su2double **val_Jacobian_i, CConfig *config)
virtual void	GetEq_Rxn_Coefficients (su2double **EqnRxnConstants, CConfig *config)
virtual void	ComputeResidual_Axisymmetric (su2double *val_residual, CConfig *config)
	Residual for source term integration. More...
virtual void	ComputeResidual_Axisymmetric_ad (su2double *val_residual, su2double *val_residuald, CConfig *config)
	Residual for source term integration. More...
virtual void	SetJacobian_Axisymmetric (su2double **val_Jacobian_i, CConfig *config)
	Calculation of axisymmetric source term Jacobian. More...
virtual void	ComputeVibRelaxation (su2double *val_residual, su2double **val_Jacobian_i, CConfig *config)
	Calculation of the translational-vibrational energy exchange source term. More...
virtual void	ComputeChemistry (su2double *val_residual, su2double **val_Jacobian_i, CConfig *config)
	Calculation of the chemistry source term. More...
virtual void	GetKeqConstants (su2double *A, unsigned short val_reaction, CConfig *config)
	Calculates constants used for Keq correlation. More...
virtual void	ComputeResidual (su2double **val_Jacobian_i, su2double *val_Jacobian_mui, su2double ***val_Jacobian_gradi, CConfig *config)
virtual void	ComputeResidual (su2double **val_Jacobian_i, su2double *val_Jacobian_mui, su2double ***val_Jacobian_gradi, su2double **val_Jacobian_j, su2double *val_Jacobian_muj, su2double ***val_Jacobian_gradj, CConfig *config)
virtual void	Compute_Tangent_Matrix (CElement *element_container, CConfig *config)
	A virtual member to compute the tangent matrix in structural problems. More...
virtual void	Compute_MeanDilatation_Term (CElement *element_container, CConfig *config)
	A virtual member to compute the pressure term in incompressible or nearly-incompressible structural problems. More...
virtual void	Compute_NodalStress_Term (CElement *element_container, CConfig *config)
	A virtual member to compute the nodal stress term in non-linear structural problems. More...
virtual void	Compute_Plane_Stress_Term (CElement *element_container, CConfig *config)
	A virtual member to compute the plane stress term in an element for nonlinear structural problems. More...
virtual void	Compute_Constitutive_Matrix (CElement *element_container, CConfig *config)
	A virtual member to compute the constitutive matrix in an element for structural problems. More...
virtual void	Compute_Stress_Tensor (CElement *element_container, CConfig *config)
	A virtual member to compute the stress tensor in an element for structural problems. More...
virtual void	Compute_Mass_Matrix (CElement *element_container, CConfig *config)
	A virtual member to compute the mass matrix. More...
virtual void	Compute_Dead_Load (CElement *element_container, CConfig *config)
	A virtual member to compute the residual component due to dead loads. More...
virtual void	Compute_Averaged_NodalStress (CElement *element_container, CConfig *config)
	A virtual member to compute the averaged nodal stresses. More...
void	CreateBasis (su2double *val_Normal)
	Computes a basis of orthogonal vectors from a suppled vector. More...

Additional Inherited Members
Public Attributes inherited from CNumerics
su2double **	Flux_Tensor
	Flux tensor (used for viscous and inviscid purposes.
su2double *	Proj_Flux_Tensor
	Flux tensor projected in a direction.
su2double **	tau
	Viscous stress tensor.
su2double **	delta
	Identity matrix.
su2double *	Diffusion_Coeff_i
	Species diffusion coefficients at point i.
su2double *	Diffusion_Coeff_j
	Species diffusion coefficients at point j.
su2double	Laminar_Viscosity_i
	Laminar viscosity at point i.
su2double	Laminar_Viscosity_j
	Laminar viscosity at point j.
su2double	Laminar_Viscosity_id
	Variation of laminar viscosity at point i.
su2double	Laminar_Viscosity_jd
	Variation of laminar viscosity at point j.
su2double	Thermal_Conductivity_i
	Thermal conductivity at point i.
su2double	Thermal_Conductivity_j
	Thermal conductivity at point j.
su2double	Thermal_Conductivity_ve_i
	Thermal conductivity at point i.
su2double	Thermal_Conductivity_ve_j
	Thermal conductivity at point j.
su2double	Cp_i
	Cp at point i.
su2double	Cp_j
	Cp at point j.
su2double *	Theta_v
	Characteristic vibrational temperature.
su2double	Eddy_Viscosity_i
	Eddy viscosity at point i.
su2double	Eddy_Viscosity_j
	Eddy viscosity at point j.
su2double	turb_ke_i
	Turbulent kinetic energy at point i.
su2double	turb_ke_j
	Turbulent kinetic energy at point j.
su2double	Pressure_i
	Pressure at point i.
su2double	Pressure_j
	Pressure at point j.
su2double	GravityForce_i
	Gravity force at point i.
su2double	GravityForce_j
	Gravity force at point j.
su2double	Density_i
	Density at point i.
su2double	Density_j
	Density at point j.
su2double	DensityInc_i
	Incompressible density at point i.
su2double	DensityInc_j
	Incompressible density at point j.
su2double	BetaInc2_i
	Beta incompressible at point i.
su2double	BetaInc2_j
	Beta incompressible at point j.
su2double	Lambda_i
	Spectral radius at point i.
su2double	Lambda_j
	Spectral radius at point j.
su2double	LambdaComb_i
	Spectral radius at point i.
su2double	LambdaComb_j
	Spectral radius at point j.
su2double	SoundSpeed_i
	Sound speed at point i.
su2double	SoundSpeed_j
	Sound speed at point j.
su2double	Enthalpy_i
	Enthalpy at point i.
su2double	Enthalpy_j
	Enthalpy at point j.
su2double	dist_i
	Distance of point i to the nearest wall.
su2double	dist_j
	Distance of point j to the nearest wall.
su2double	Temp_i
	Temperature at point i.
su2double	Temp_j
	Temperature at point j.
su2double *	Temp_tr_i
	Temperature transl-rot at point i.
su2double *	Temp_tr_j
	Temperature transl-rot at point j.
su2double *	Temp_vib_i
	Temperature vibrational at point i.
su2double *	Temp_vib_j
	Temperature vibrational at point j.
su2double *	Und_Lapl_i
	Undivided laplacians at point i.
su2double *	Und_Lapl_j
	Undivided laplacians at point j.
su2double	Sensor_i
	Pressure sensor at point i.
su2double	Sensor_j
	Pressure sensor at point j.
su2double *	GridVel_i
	Grid velocity at point i.
su2double *	GridVel_j
	Grid velocity at point j.
su2double *	U_i
	Vector of conservative variables at point i.
su2double *	U_id
	Vector of derivative of conservative variables at point i.
su2double *	UZeroOrder_i
	Vector of conservative variables at point i without reconstruction.
su2double *	U_j
	Vector of conservative variables at point j.
su2double *	UZeroOrder_j
	Vector of conservative variables at point j without reconstruction.
su2double *	U_jd
	Vector of derivative of conservative variables at point j.
su2double *	U_0
	Vector of conservative variables at node 0.
su2double *	U_1
	Vector of conservative variables at node 1.
su2double *	U_2
	Vector of conservative variables at node 2.
su2double *	U_3
	Vector of conservative variables at node 3.
su2double *	V_i
	Vector of primitive variables at point i.
su2double *	V_j
	Vector of primitive variables at point j.
su2double *	S_i
	Vector of secondary variables at point i.
su2double *	S_j
	Vector of secondary variables at point j.
su2double *	Psi_i
	Vector of adjoint variables at point i.
su2double *	Psi_j
	Vector of adjoint variables at point j.
su2double *	DeltaU_i
	Vector of linearized variables at point i.
su2double *	DeltaU_j
	Vector of linearized variables at point j.
su2double *	TurbVar_i
	Vector of turbulent variables at point i.
su2double *	TurbVar_id
	Vector of derivative of turbulent variables at point i.
su2double *	TurbVar_j
	Vector of turbulent variables at point j.
su2double *	TurbVar_jd
	Vector of derivative of turbulent variables at point j.
su2double *	TransVar_i
	Vector of turbulent variables at point i.
su2double *	TransVar_j
	Vector of turbulent variables at point j.
su2double *	TurbPsi_i
	Vector of adjoint turbulent variables at point i.
su2double *	TurbPsi_j
	Vector of adjoint turbulent variables at point j.
su2double **	ConsVar_Grad_i
	Gradient of conservative variables at point i.
su2double **	ConsVar_Grad_j
	Gradient of conservative variables at point j.
su2double **	ConsVar_Grad_0
	Gradient of conservative variables at point 0.
su2double **	ConsVar_Grad_1
	Gradient of conservative variables at point 1.
su2double **	ConsVar_Grad_2
	Gradient of conservative variables at point 2.
su2double **	ConsVar_Grad_3
	Gradient of conservative variables at point 3.
su2double **	ConsVar_Grad
	Gradient of conservative variables which is a scalar.
su2double **	PrimVar_Grad_i
	Gradient of primitive variables at point i.
su2double **	PrimVar_Grad_j
	Gradient of primitive variables at point j.
su2double *	PrimVar_Lim_i
	Limiter of primitive variables at point i.
su2double *	PrimVar_Lim_j
	Limiter of primitive variables at point j.
su2double *	PsiVar_Lim_i
	Limiter of adjoint variables at point i.
su2double *	PsiVar_Lim_j
	Limiter of adjoint variables at point j.
su2double **	PsiVar_Grad_i
	Gradient of adjoint variables at point i.
su2double **	PsiVar_Grad_j
	Gradient of adjoint variables at point j.
su2double **	TurbVar_Grad_i
	Gradient of turbulent variables at point i.
su2double **	TurbVar_Grad_j
	Gradient of turbulent variables at point j.
su2double **	TransVar_Grad_i
	Gradient of turbulent variables at point i.
su2double **	TransVar_Grad_j
	Gradient of turbulent variables at point j.
su2double **	TurbPsi_Grad_i
	Gradient of adjoint turbulent variables at point i.
su2double **	TurbPsi_Grad_j
	Gradient of adjoint turbulent variables at point j.
su2double *	AuxVar_Grad_i
	Gradient of an auxiliary variable at point i.
su2double *	AuxVar_Grad_j
	Gradient of an auxiliary variable at point i.
su2double *	Coord_i
	Cartesians coordinates of point i.
su2double *	Coord_j
	Cartesians coordinates of point j.
su2double *	Coord_0
	Cartesians coordinates of point 0 (Galerkin method, triangle).
su2double *	Coord_1
	Cartesians coordinates of point 1 (Galerkin method, tetrahedra).
su2double *	Coord_2
	Cartesians coordinates of point 2 (Galerkin method, triangle).
su2double *	Coord_3
	Cartesians coordinates of point 3 (Galerkin method, tetrahedra).
unsigned short	Neighbor_i
	Number of neighbors of the point i.
unsigned short	Neighbor_j
	Number of neighbors of the point j.
su2double *	Normal
	Normal vector, it norm is the area of the face.
su2double *	UnitNormal
	Unitary normal vector.
su2double *	UnitNormald
	derivatve of unitary normal vector.
su2double	TimeStep
	Time step useful in dual time method.
su2double	Area
	Area of the face i-j.
su2double	Volume
	Volume of the control volume around point i.
su2double	Volume_n
	Volume of the control volume at time n.
su2double	Volume_nM1
	Volume of the control volume at time n-1.
su2double	Volume_nP1
	Volume of the control volume at time n+1.
su2double *	U_n
	Vector of conservative variables at time n.
su2double *	U_nM1
	Vector of conservative variables at time n-1.
su2double *	U_nP1
	Vector of conservative variables at time n+1.
su2double	vel2_inf
	value of the square of freestream speed.
su2double *	WindGust_i
	Wind gust at point i.
su2double *	WindGust_j
	Wind gust at point j.
su2double *	WindGustDer_i
	Wind gust derivatives at point i.
su2double *	WindGustDer_j
	Wind gust derivatives at point j.
su2double *	Vorticity_i
su2double *	Vorticity_j
	Vorticity.
su2double	StrainMag_i
su2double	StrainMag_j
	Strain rate magnitude.
su2double *	l
su2double *	m
Protected Attributes inherited from CNumerics
unsigned short	nDim
unsigned short	nVar
	Number of dimensions and variables.
su2double	Gamma
	Fluid's Gamma constant (ratio of specific heats).
su2double	Gamma_Minus_One
	Fluids's Gamma - 1.0 .
su2double	Gas_Constant
	Gas constant.
su2double *	Vector
	Auxiliary vector.
su2double *	Enthalpy_formation
su2double	Prandtl_Lam
	Laminar Prandtl's number.
su2double	Prandtl_Turb
	Turbulent Prandtl's number.

Detailed Description

Class for integrating the source terms of the Spalart-Allmaras turbulence model equation.

Author

A. Bueno.

Version

5.0.0 "Raven"

Constructor & Destructor Documentation

CSourcePieceWise_TurbSA()

CSourcePieceWise_TurbSA::CSourcePieceWise_TurbSA	(	unsigned short	val_nDim,
		unsigned short	val_nVar,
		CConfig *	config
	)

Constructor of the class.

Parameters

[in]	val_nDim	- Number of dimensions of the problem.
[in]	val_nVar	- Number of variables of the problem.
[in]	config	- Definition of the particular problem.

Member Function Documentation

ComputeResidual()

void CSourcePieceWise_TurbSA::ComputeResidual ( su2double *  val_residual, su2double **  val_Jacobian_i, su2double **  val_Jacobian_j, CConfig *  config  )

virtual

Residual for source term integration.

Parameters

[out]	val_residual	- Pointer to the total residual.
[out]	val_Jacobian_i	- Jacobian of the numerical method at node i (implicit computation).
[out]	val_Jacobian_j	- Jacobian of the numerical method at node j (implicit computation).
[in]	config	- Definition of the particular problem.

Reimplemented from CNumerics.

SetCrossProduction()

void CSourcePieceWise_TurbSA::SetCrossProduction ( su2double  val_crossproduction )

inlinevirtual

Residual for source term integration.

Parameters

[in]

val_crossproduction

- Value of the CrossProduction.

Reimplemented from CNumerics.

SetDestruction()

void CSourcePieceWise_TurbSA::SetDestruction ( su2double  val_destruction )

inlinevirtual

Residual for source term integration.

Parameters

[in]

val_destruction

- Value of the Destruction.

Reimplemented from CNumerics.

SetIntermittency()

void CSourcePieceWise_TurbSA::SetIntermittency ( su2double  intermittency_in )

inlinevirtual

Residual for source term integration.

Parameters

[in]

intermittency_in

- Value of the intermittency.

Reimplemented from CNumerics.

SetProduction()

void CSourcePieceWise_TurbSA::SetProduction ( su2double  val_production )

inlinevirtual

Residual for source term integration.

Parameters

[in]

val_production

- Value of the Production.

Reimplemented from CNumerics.

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The documentation for this class was generated from the following files:

• SU2_CFD/include/numerics_structure.hpp
• SU2_CFD/include/numerics_structure.inl
• SU2_CFD/src/numerics_direct_turbulent.cpp