CNumerics Class Reference

Class for defining the numerical methods. More...

#include <numerics_structure.hpp>

Inheritance diagram for CNumerics:

Public Member Functions
	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, 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	SetIntermittency (su2double intermittency_in)
	Set intermittency for numerics (used in SA with LM transition model)
virtual void	SetProduction (su2double val_production)
	Residual for source term integration. More...
virtual void	SetDestruction (su2double val_destruction)
	Residual for source term integration. More...
virtual void	SetCrossProduction (su2double val_crossproduction)
	Residual for source term integration. More...
virtual su2double	GetProduction (void)
	Residual for source term integration. More...
virtual su2double	GetDestruction (void)
	Residual for source term integration. More...
virtual su2double	GetCrossProduction (void)
	Residual for source term integration. 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...

Public Attributes
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
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 defining the numerical methods.

Author

F. Palacios, T. Economon

Version

5.0.0 "Raven"

Constructor & Destructor Documentation

CNumerics()

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

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

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

Compute_Averaged_NodalStress()

void CNumerics::Compute_Averaged_NodalStress ( CElement *  element_container, CConfig *  config  )

inlinevirtual

A virtual member to compute the averaged nodal stresses.

Parameters

[in]

element_container

- Element structure for the particular element integrated.

Reimplemented in CFEM_NonlinearElasticity, CFEM_LinearElasticity, and CFEM_Elasticity.

Compute_Constitutive_Matrix()

void CNumerics::Compute_Constitutive_Matrix ( CElement *  element_container, CConfig *  config  )

inlinevirtual

A virtual member to compute the constitutive matrix in an element for structural problems.

Parameters

[in]

element_container

- Element structure for the particular element integrated.

Reimplemented in CFEM_NeoHookean_Incomp, CFEM_NeoHookean_Comp, CFEM_NonlinearElasticity, and CFEM_Elasticity.

Compute_Dead_Load()

void CNumerics::Compute_Dead_Load ( CElement *  element_container, CConfig *  config  )

inlinevirtual

A virtual member to compute the residual component due to dead loads.

Parameters

[in]

element_container

- Element structure for the particular element integrated.

Reimplemented in CFEM_Elasticity.

Compute_Mass_Matrix()

void CNumerics::Compute_Mass_Matrix ( CElement *  element_container, CConfig *  config  )

inlinevirtual

A virtual member to compute the mass matrix.

Parameters

[in]

element_container

- Element structure for the particular element integrated.

Reimplemented in CFEM_Elasticity.

Compute_MeanDilatation_Term()

void CNumerics::Compute_MeanDilatation_Term ( CElement *  element_container, CConfig *  config  )

inlinevirtual

A virtual member to compute the pressure term in incompressible or nearly-incompressible structural problems.

Parameters

[in]

element_container

- Definition of the particular element integrated.

Reimplemented in CFEM_NonlinearElasticity, and CFEM_Elasticity.

Compute_NodalStress_Term()

void CNumerics::Compute_NodalStress_Term ( CElement *  element_container, CConfig *  config  )

inlinevirtual

A virtual member to compute the nodal stress term in non-linear structural problems.

Parameters

[in]

element_container

- Definition of the particular element integrated.

Reimplemented in CFEM_NonlinearElasticity, and CFEM_Elasticity.

Compute_Plane_Stress_Term()

void CNumerics::Compute_Plane_Stress_Term ( CElement *  element_container, CConfig *  config  )

inlinevirtual

A virtual member to compute the plane stress term in an element for nonlinear structural problems.

Parameters

[in]

element_container

- Element structure for the particular element integrated.

Reimplemented in CFEM_NeoHookean_Incomp, CFEM_NeoHookean_Comp, CFEM_NonlinearElasticity, and CFEM_Elasticity.

Compute_Stress_Tensor()

void CNumerics::Compute_Stress_Tensor ( CElement *  element_container, CConfig *  config  )

inlinevirtual

A virtual member to compute the stress tensor in an element for structural problems.

Parameters

[in]

element_container

- Element structure for the particular element integrated.

Reimplemented in CFEM_NeoHookean_Incomp, CFEM_NeoHookean_Comp, CFEM_NonlinearElasticity, and CFEM_Elasticity.

Compute_Tangent_Matrix()

void CNumerics::Compute_Tangent_Matrix ( CElement *  element_container, CConfig *  config  )

inlinevirtual

A virtual member to compute the tangent matrix in structural problems.

Parameters

[in]

element_container

- Element structure for the particular element integrated.

Reimplemented in CFEM_NonlinearElasticity, CFEM_LinearElasticity, and CFEM_Elasticity.

ComputeChemistry()

void CNumerics::ComputeChemistry ( su2double *  val_residual, su2double **  val_Jacobian_i, CConfig *  config  )

inlinevirtual

Calculation of the chemistry source term.

Parameters

[in]	config	- Definition of the particular problem.
[out]	val_residual	- residual of the source terms
[out]	val_Jacobian_i	- Jacobian of the source terms

ComputeResidual() [1/13]

void CNumerics::ComputeResidual ( su2double *  val_residual, CConfig *  config  )

inlinevirtual

Compute the numerical residual.

Parameters

[out]	val_residual	- Pointer to the total residual.
[in]	config	- Definition of the particular problem.

Reimplemented in CSourceConservative_AdjFlow, CSourceViscous_AdjFlow, and CSourceGravity.

ComputeResidual() [2/13]

void CNumerics::ComputeResidual ( su2double *  val_residual_i, su2double *  val_residual_j  )

inlinevirtual

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[out]	val_residual_i	- Pointer to the total residual at point i.
[out]	val_residual_j	- Pointer to the total residual at point j.

ComputeResidual() [3/13]

void CNumerics::ComputeResidual ( su2double *  val_residual_i, su2double *  val_residual_j, CConfig *  config  )

inlinevirtual

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[out]	val_residual_i	- Pointer to the total residual at point i.
[out]	val_residual_j	- Pointer to the total residual at point j.
[in]	config	- Definition of the particular problem.

ComputeResidual() [4/13]

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

inlinevirtual

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

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 in CViscous_Template, CConvective_Template, CSourceConservative_AdjTurb, CSourcePieceWise_AdjTurb, CSourcePieceWise_TurbSST, CSourcePieceWise_TurbSA_Neg, CSourcePieceWise_TurbSA, CAvgGrad_AdjTurb, CAvgGradCorrected_AdjTurb, CAvgGradCorrected_TurbSST, CAvgGrad_TurbSST, CAvgGradCorrected_TransLM, CAvgGradCorrected_TurbML, CAvgGradCorrected_TurbSA_Neg, CAvgGradCorrected_TurbSA, CAvgGradCorrectedArtComp_Flow, CGeneralAvgGradCorrected_Flow, CAvgGradCorrected_Flow, CAvgGrad_TransLM, CAvgGrad_TurbML, CAvgGrad_TurbSA_Neg, CAvgGrad_TurbSA, CAvgGradArtComp_Flow, CGeneralAvgGrad_Flow, CAvgGrad_Flow, CCentLaxArtComp_Flow, CCentLax_Flow, CCentJSTArtComp_Flow, CCentJST_Flow, CCentJST_KE_Flow, CUpwSca_TransLM, CUpwSca_TurbSST, CUpwSca_TurbML, CUpwSca_TurbSA, CUpwLin_AdjTurb, CUpwLin_TransLM, CUpwGeneralHLLC_Flow, CUpwHLLC_Flow, CUpwAUSM_Flow, CUpwArtComp_Flow, CUpwTurkel_Flow, CUpwMSW_Flow, CUpwGeneralRoe_Flow, CUpwRoe_Flow, and CUpwCUSP_Flow.

ComputeResidual() [5/13]

void CNumerics::ComputeResidual ( su2double *  val_residual, su2double **  val_Jacobian_i, su2double **  val_Jacobian_j, su2double **  val_JacobianMeanFlow_i, su2double **  val_JacobianMeanFlow_j, CConfig *  config  )

inlinevirtual

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

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).
[out]	val_JacobianMeanFlow_i	- Jacobian of the numerical method at node i (implicit computation).
[out]	val_JacobianMeanFlow_j	- Jacobian of the numerical method at node j (implicit computation).
[in]	config	- Definition of the particular problem.

ComputeResidual() [6/13]

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

inlinevirtual

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[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.

ComputeResidual() [7/13]

void CNumerics::ComputeResidual ( su2double *  val_resconv, su2double *  val_resvisc, su2double **  val_Jacobian_i, su2double **  val_Jacobian_j, CConfig *  config  )

inlinevirtual

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[out]	val_resconv	- Pointer to the convective residual.
[out]	val_resvisc	- Pointer to the artificial viscosity 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.

ComputeResidual() [8/13]

void CNumerics::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  )

inlinevirtual

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[out]	val_residual_i	- Pointer to the total residual at point i.
[out]	val_residual_j	- Pointer to the total viscosity residual at point j.
[out]	val_Jacobian_ii	- Jacobian of the numerical method at node i (implicit computation) from node i.
[out]	val_Jacobian_ij	- Jacobian of the numerical method at node i (implicit computation) from node j.
[out]	val_Jacobian_ji	- Jacobian of the numerical method at node j (implicit computation) from node i.
[out]	val_Jacobian_jj	- Jacobian of the numerical method at node j (implicit computation) from node j.
[in]	config	- Definition of the particular problem.

Reimplemented in CAvgGrad_AdjTurb, CAvgGradCorrected_AdjTurb, CAvgGradCorrectedArtComp_AdjFlow, CAvgGradCorrected_AdjFlow, CAvgGradArtComp_AdjFlow, CAvgGrad_AdjFlow, CUpwSca_AdjTurb, CUpwRoeArtComp_AdjFlow, and CUpwRoe_AdjFlow.

ComputeResidual() [9/13]

void CNumerics::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  )

inlinevirtual

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[out]	val_resconv_i	- Pointer to the convective residual at point i.
[out]	val_resvisc_i	- Pointer to the artificial viscosity residual at point i.
[out]	val_resconv_j	- Pointer to the convective residual at point j.
[out]	val_resvisc_j	- Pointer to the artificial viscosity residual at point j.
[out]	val_Jacobian_ii	- Jacobian of the numerical method at node i (implicit computation) from node i.
[out]	val_Jacobian_ij	- Jacobian of the numerical method at node i (implicit computation) from node j.
[out]	val_Jacobian_ji	- Jacobian of the numerical method at node j (implicit computation) from node i.
[out]	val_Jacobian_jj	- Jacobian of the numerical method at node j (implicit computation) from node j.
[in]	config	- Definition of the particular problem.

Reimplemented in CCentLaxArtComp_AdjFlow, CCentLax_AdjFlow, CCentJSTArtComp_AdjFlow, and CCentJST_AdjFlow.

ComputeResidual() [10/13]

void CNumerics::ComputeResidual ( su2double **  val_stiffmatrix_elem, CConfig *  config  )

inlinevirtual

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[out]	val_stiffmatrix_elem	- Stiffness matrix for Galerkin computation.
[in]	config	- Definition of the particular problem.

Reimplemented in CGalerkin_Flow.

ComputeResidual() [11/13]

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

inlinevirtual

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[in]	config	- Definition of the particular problem.
[out]	val_residual	- residual of the source terms
[out]	val_Jacobian_i	- Jacobian of the source terms

Reimplemented in CSource_Template, CSourceWindGust, CSourceAxisymmetric_AdjFlow, CSourceAxisymmetric_Flow, CSourceRotatingFrame_AdjFlow, and CSourceRotatingFrame_Flow.

ComputeResidual() [12/13]

void CNumerics::ComputeResidual ( su2double **  val_Jacobian_i, su2double *  val_Jacobian_mui, su2double ***  val_Jacobian_gradi, CConfig *  config  )

inlinevirtual

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[out]	val_Jacobian_i	- Jacobian of the numerical method at node i
[in]	config	- Definition of the particular problem.

ComputeResidual() [13/13]

void CNumerics::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  )

inlinevirtual

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[out]	val_Jacobian_i	- Jacobian of the numerical method at node i
[in]	config	- Definition of the particular problem.

ComputeResidual_Axisymmetric()

void CNumerics::ComputeResidual_Axisymmetric ( su2double *  val_residual, CConfig *  config  )

inlinevirtual

Residual for source term integration.

Parameters

[out]	val_residual	- Pointer to the source residual containing chemistry terms.
[in]	config	- Definition of the particular problem.

ComputeResidual_Axisymmetric_ad()

void CNumerics::ComputeResidual_Axisymmetric_ad ( su2double *  val_residual, su2double *  val_residuald, CConfig *  config  )

inlinevirtual

Residual for source term integration.

Parameters

[out]	val_residual	- Pointer to the source residual containing chemistry terms.
[in]	config	- Definition of the particular problem.

ComputeVibRelaxation()

void CNumerics::ComputeVibRelaxation ( su2double *  val_residual, su2double **  val_Jacobian_i, CConfig *  config  )

inlinevirtual

Calculation of the translational-vibrational energy exchange source term.

Parameters

[in]	config	- Definition of the particular problem.
[out]	val_residual	- residual of the source terms
[out]	val_Jacobian_i	- Jacobian of the source terms

CreateBasis()

void CNumerics::CreateBasis

(

su2double *

val_Normal

)

Computes a basis of orthogonal vectors from a suppled vector.

Parameters

[in]

config

- Normal vector

Determinant_3x3()

su2double CNumerics::Determinant_3x3 ( su2double  A00, su2double  A01, su2double  A02, su2double  A10, su2double  A11, su2double  A12, su2double  A20, su2double  A21, su2double  A22  )

inline

Compute the determinant of a 3 by 3 matrix.

Parameters

[in]

val_matrix

3 by 3 matrix.

Returns

Determinant of the matrix

GetCrossProduction()

su2double CNumerics::GetCrossProduction ( void  )

inlinevirtual

Residual for source term integration.

Parameters

[in]

val_crossproduction

- Value of the CrossProduction.

Reimplemented in CSourcePieceWise_TurbSA_Neg, and CSourcePieceWise_TurbSA.

GetDestruction()

su2double CNumerics::GetDestruction ( void  )

inlinevirtual

Residual for source term integration.

Parameters

[in]

val_destruction

- Value of the Destruction.

Reimplemented in CSourcePieceWise_TurbSA_Neg, and CSourcePieceWise_TurbSA.

GetEq_Rxn_Coefficients()

void CNumerics::GetEq_Rxn_Coefficients ( su2double **  EqnRxnConstants, CConfig *  config  )

inlinevirtual

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[out]	-	Matrix for storing the constants to be used in the calculation of the equilibrium extent of reaction Keq.
[in]	config	- Definition of the particular problem.

GetInviscidArtCompProjFlux()

void CNumerics::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.

Parameters

[in]	val_density	- Pointer to the density.
[in]	val_velocity	- Pointer to the velocity.
[in]	val_pressure	- Pointer to the pressure.
[in]	val_betainc2	- Value of the artificial compresibility factor.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[out]	val_Proj_Flux	- Pointer to the projected flux.

GetInviscidArtCompProjJac()

void CNumerics::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).

Parameters

[in]	val_density	- Value of the density.
[in]	val_velocity	- Pointer to the velocity.
[in]	val_betainc2	- Value of the artificial compresibility factor.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[in]	val_scale	- Scale of the projection.
[out]	val_Proj_Jac_tensor	- Pointer to the projected inviscid Jacobian.

GetInviscidFlux()

void CNumerics::GetInviscidFlux	(	su2double	val_density,
		su2double *	val_velocity,
		su2double	val_pressure,
		su2double	val_enthalpy
	)

Get the inviscid fluxes.

Parameters

[in]	val_density	- Value of the density.
[in]	val_velocity	- Value of the velocity.
[in]	val_pressure	- Value of the pressure.
[in]	val_enthalpy	- Value of the enthalpy.

GetInviscidProjFlux()

void CNumerics::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.

Parameters

[in]	val_density	- Pointer to the density.
[in]	val_velocity	- Pointer to the velocity.
[in]	val_pressure	- Pointer to the pressure.
[in]	val_enthalpy	- Pointer to the enthalpy.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[out]	val_Proj_Flux	- Pointer to the projected flux.

GetInviscidProjJac() [1/2]

void CNumerics::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.

Parameters

[in]	val_velocity	Pointer to the velocity.
[in]	val_energy	Value of the energy.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[in]	val_scale	- Scale of the projection.
[out]	val_Proj_Jac_tensor	- Pointer to the projected inviscid Jacobian.

GetInviscidProjJac() [2/2]

void CNumerics::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.

Parameters

[in]	val_velocity	Pointer to the velocity.
[in]	val_energy	Value of the energy.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[in]	val_scale	- Scale of the projection.
[out]	val_Proj_Jac_tensor	- Pointer to the projected inviscid Jacobian.

GetinvRinvPe()

void CNumerics::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.

Parameters

[in]	Beta2	- A variable in used to define Pe matrix.
[in]	val_enthalpy	- value of the enthalpy.
[in]	val_soundspeed	- value of the sound speed.
[in]	val_density	- value of the density.
[in]	val_velocity	- value of the velocity.
[out]	val_invR_invPe	- Pointer to the matrix of conversion from entropic to conserved variables.

GetJacInviscidLambda_fabs()

void CNumerics::GetJacInviscidLambda_fabs	(	su2double *	val_velocity,
		su2double	val_soundspeed,
		su2double *	val_normal,
		su2double *	val_Lambda_Vector
	)

Computation of the projected inviscid lambda (eingenvalues).

Parameters

[in]	val_velocity	- Value of the velocity.
[in]	val_soundspeed	- Value of the sound speed.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[in]	val_Lambda_Vector	- Pointer to Lambda matrix.

GetKeqConstants()

void CNumerics::GetKeqConstants ( su2double *  A, unsigned short  val_reaction, CConfig *  config  )

inlinevirtual

Calculates constants used for Keq correlation.

Parameters

[out]	A	- Pointer to coefficient array.
[in]	val_reaction	- Reaction number indicator.
[in]	config	- Definition of the particular problem.

GetLMatrix()

void CNumerics::GetLMatrix	(	su2double	val_soundspeed,
		su2double	val_density,
		su2double *	val_normal,
		su2double **	L_Matrix
	)

Computation of the matrix R.

Parameters

[in]	val_soundspeed	- value of the sound speed.
[in]	val_density	- value of the density.
[in]	val_normal	- value of the unit normal.
[out]	L_Matrix	- Pointer to the matrix of conversion from conserved to entropic variables.

GetPArtCompMatrix()

void CNumerics::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 $P^{-1}(A.Normal)P=Lambda$.

Parameters

[in]	val_density	- Value of the density.
[in]	val_velocity	- Value of the velocity.
[in]	val_betainv2	- Value of the compresibility factor.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[out]	val_p_tensor	- Pointer to the P matrix.

GetPArtCompMatrix_inv()

void CNumerics::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 $P^{-1}(A.Normal)P=Lambda$.

Parameters

[in]	val_density	- Value of the density.
[in]	val_velocity	- Value of the velocity.
[in]	val_betainv2	- Value of the compresibility factor.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[out]	val_invp_tensor	- Pointer to inverse of the P matrix.

GetPMatrix() [1/2]

void CNumerics::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.

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[in]	val_density	- Value of the density.
[in]	val_velocity	- Value of the velocity.
[in]	val_soundspeed	- Value of the sound speed.
[in]	val_enthalpy	- Value of the Enthalpy
[in]	val_chi	- Value of the derivative of Pressure with respect to the Density.
[in]	val_kappa	- Value of the derivative of Pressure with respect to the volume specific Static Energy.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[out]	val_p_tensor	- Pointer to the P matrix.

GetPMatrix() [2/2]

void CNumerics::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 $P^{-1}(A.Normal)P=Lambda$.

Parameters

[in]	val_density	- Value of the density.
[in]	val_velocity	- Value of the velocity.
[in]	val_soundspeed	- Value of the sound speed.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[out]	val_p_tensor	- Pointer to the P matrix.

GetPMatrix_inv() [1/2]

void CNumerics::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 $P^{-1}(A.Normal)P=Lambda$.

Parameters

[in]	val_density	- Value of the density.
[in]	val_velocity	- Value of the velocity.
[in]	val_soundspeed	- Value of the sound speed.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[out]	val_invp_tensor	- Pointer to inverse of the P matrix.

GetPMatrix_inv() [2/2]

void CNumerics::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 $P^{-1}(A.Normal)P=Lambda$.

Parameters

[in]	val_density	- Value of the density.
[in]	val_velocity	- Value of the velocity.
[in]	val_soundspeed	- Value of the sound speed.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[out]	val_invp_tensor	- Pointer to inverse of the P matrix.

GetPrecond_Beta()

su2double CNumerics::GetPrecond_Beta ( )

inlinevirtual

Get the Preconditioning Beta.

Returns

val_Beta - Value of the low Mach Preconditioner.

Reimplemented in CUpwTurkel_Flow.

GetPrecondJacobian()

void CNumerics::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 $Tg |Lambda| Td = Pc{-1}|Pc (A.Normal)|$.

Parameters

[in]	Beta2	- A variable in used to define absPeJacobian matrix.
[in]	r_hat	- A variable in used to define absPeJacobian matrix.
[in]	s_hat	- A variable in used to define absPeJacobian matrix.
[in]	t_hat	- A variable in used to define absPeJacobian matrix.
[in]	rB2a2	- A variable in used to define absPeJacobian matrix.
[in]	val_Lambda	- Eigenvalues of the Preconditioned Jacobian.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[out]	val_absPeJac	- Pointer to the Preconditioned Jacobian matrix.

GetPrimitive2Conservative()

void CNumerics::GetPrimitive2Conservative	(	su2double *	val_Mean_PrimVar,
		su2double *	val_Mean_SecVar,
		su2double **	val_Jac_PC
	)

Mapping between primitives variables P and conservatives variables C.

Parameters

[in]	val_Mean_PrimVar	- Mean value of the primitive variables.
[in]	val_Mean_PrimVar	- Mean Value of the secondary variables.
[out]	val_Jac_PC	- Pointer to the Jacobian dPdC.

GetProduction()

su2double CNumerics::GetProduction ( void  )

inlinevirtual

Residual for source term integration.

Parameters

[in]

val_production

- Value of the Production.

Reimplemented in CSourcePieceWise_TurbSA_Neg, and CSourcePieceWise_TurbSA.

GetRMatrix() [1/2]

void CNumerics::GetRMatrix	(	su2double	val_pressure,
		su2double	val_soundspeed,
		su2double	val_density,
		su2double *	val_velocity,
		su2double **	val_invR_invPe
	)

Computation of the matrix R.

Parameters

[in]	val_pressure	- value of the pressure.
[in]	val_soundspeed	- value of the sound speed.
[in]	val_density	- value of the density.
[in]	val_velocity	- value of the velocity.
[out]	val_invR_invPe	- Pointer to the matrix of conversion from entropic to conserved variables.

GetRMatrix() [2/2]

void CNumerics::GetRMatrix	(	su2double	val_soundspeed,
		su2double	val_density,
		su2double *	val_normal,
		su2double **	R_Matrix
	)

Computation of the matrix R.

Parameters

[in]	val_soundspeed	- value of the sound speed.
[in]	val_density	- value of the density.
[in]	val_normal	- value of the unit normal.
[out]	R_Matrix	- Pointer to the matrix of conversion from entropic to conserved variables.

GetViscousArtCompProjJacs()

void CNumerics::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.

Parameters

[in]	val_laminar_viscosity	- Value of the laminar viscosity.
[in]	val_eddy_viscosity	- Value of the eddy viscosity.
[in]	val_dist_ij	- Distance between the points.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[in]	val_dS	- Area of the face between two nodes.
[out]	val_Proj_Jac_Tensor_i	- Pointer to the projected viscous Jacobian at point i.
[out]	val_Proj_Jac_Tensor_j	- Pointer to the projected viscous Jacobian at point j.

GetViscousFlux()

void CNumerics::GetViscousFlux	(	su2double *	val_primvar,
		su2double **	val_gradprimvar,
		su2double	val_laminar_viscosity,
		su2double	val_eddy_viscosity,
		su2double	val_mach_inf
	)

Get the viscous fluxes.

Parameters

[in]	val_primvar	- Value of the primitive variables.
[in]	val_gradprimvar	- Gradient of the primitive variables.
[in]	val_laminar_viscosity	- Value of the laminar viscosity.
[in]	val_eddy_viscosity	- Value of the eddy viscosity.
[in]	val_mach_inf	- Value of the Mach number at the infinity.

GetViscousProjFlux() [1/2]

void CNumerics::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.

Parameters

[in]	val_primvar	- Primitive variables.
[in]	val_gradprimvar	- Gradient of the primitive variables.
[in]	val_turb_ke	- Turbulent kinetic energy
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[in]	val_laminar_viscosity	- Laminar viscosity.
[in]	val_eddy_viscosity	- Eddy viscosity.
[in]	val_thermal_conductivity	- Thermal Conductivity.
[in]	val_eddy_conductivity	- Eddy Conductivity.

GetViscousProjFlux() [2/2]

void CNumerics::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.

Parameters

[in]	val_primvar	- Primitive variables.
[in]	val_gradprimvar	- Gradient of the primitive variables.
[in]	val_turb_ke	- Turbulent kinetic energy
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[in]	val_laminar_viscosity	- Laminar viscosity.
[in]	val_eddy_viscosity	- Eddy viscosity.
[in]	val_thermal_conductivity	- Thermal Conductivity.
[in]	val_heat_capacity_cp	- Heat Capacity at constant pressure.

GetViscousProjJacs() [1/2]

void CNumerics::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.

Parameters

[in]	val_Mean_PrimVar	- Mean value of the primitive variables.
[in]	val_laminar_viscosity	- Value of the laminar viscosity.
[in]	val_eddy_viscosity	- Value of the eddy viscosity.
[in]	val_dist_ij	- Distance between the points.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[in]	val_dS	- Area of the face between two nodes.
[in]	val_Proj_Visc_Flux	- Pointer to the projected viscous flux.
[out]	val_Proj_Jac_Tensor_i	- Pointer to the projected viscous Jacobian at point i.
[out]	val_Proj_Jac_Tensor_j	- Pointer to the projected viscous Jacobian at point j.

GetViscousProjJacs() [2/2]

void CNumerics::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.

Parameters

[in]	val_Mean_PrimVar	- Mean value of the primitive variables.
[in]	val_gradprimvar	- Mean value of the gradient of the primitive variables.
[in]	val_Mean_SecVar	- Mean value of the secondary variables.
[in]	val_laminar_viscosity	- Value of the laminar viscosity.
[in]	val_eddy_viscosity	- Value of the eddy viscosity.
[in]	val_thermal_conductivity	- Value of the thermal conductivity.
[in]	val_heat_capacity_cp	- Value of the specific heat at constant pressure.
[in]	val_dist_ij	- Distance between the points.
[in]	val_normal	- Normal vector, the norm of the vector is the area of the face.
[in]	val_dS	- Area of the face between two nodes.
[in]	val_Proj_Visc_Flux	- Pointer to the projected viscous flux.
[out]	val_Proj_Jac_Tensor_i	- Pointer to the projected viscous Jacobian at point i.
[out]	val_Proj_Jac_Tensor_j	- Pointer to the projected viscous Jacobian at point j.

SetAdjointVar()

void CNumerics::SetAdjointVar ( su2double *  val_psi_i, su2double *  val_psi_j  )

inline

Set the value of the adjoint variable.

Parameters

[in]	val_psi_i	- Value of the adjoint variable at point i.
[in]	val_psi_j	- Value of the adjoint variable at point j.

SetAdjointVarGradient()

void CNumerics::SetAdjointVarGradient ( su2double **  val_psivar_grad_i, su2double **  val_psivar_grad_j  )

inline

Set the gradient of the adjoint variables.

Parameters

[in]	val_psivar_grad_i	- Gradient of the adjoint variable at point i.
[in]	val_psivar_grad_j	- Gradient of the adjoint variable at point j.

SetAdjointVarLimiter()

void CNumerics::SetAdjointVarLimiter ( su2double *  val_psivar_lim_i, su2double *  val_psivar_lim_j  )

inline

Set the limiter of the adjoint variables.

Parameters

[in]	val_psivar_lim_i	- Gradient of the adjoint variable at point i.
[in]	val_psivar_lim_j	- Gradient of the adjoint variable at point j.

SetAIndex()

void CNumerics::SetAIndex

(

unsigned short

val_Index

)

Retrieves the value of the species density in the primitive variable vector.

Parameters

[in]

iRho_s

SetAuxVarGrad()

void CNumerics::SetAuxVarGrad ( su2double *  val_auxvargrad_i, su2double *  val_auxvargrad_j  )

inline

Set the gradient of the auxiliary variables.

Parameters

[in]	val_auxvargrad_i	- Gradient of the auxiliary variable at point i.
[in]	val_auxvargrad_j	- Gradient of the auxiliary variable at point j.

SetBetaInc2()

void CNumerics::SetBetaInc2 ( su2double  val_betainc2_i, su2double  val_betainc2_j  )

inline

Set the value of the beta for incompressible flows.

Parameters

[in]	val_betainc2_i	- Value of beta for incompressible flows at point i.
[in]	val_betainc2_j	- Value of beta for incompressible flows at point j.

SetConservative() [1/3]

void CNumerics::SetConservative ( su2double *  val_u_i, su2double *  val_u_j  )

inline

Set the value of the conservative variables.

Parameters

[in]	val_u_i	- Value of the conservative variable at point i.
[in]	val_u_j	- Value of the conservative variable at point j.

SetConservative() [2/3]

void CNumerics::SetConservative ( su2double *  val_u_0, su2double *  val_u_1, su2double *  val_u_2  )

inline

Set the value of the conservative variables.

Parameters

[in]	val_u_0	- Value of the conservative variable at point 0.
[in]	val_u_1	- Value of the conservative variable at point 1.
[in]	val_u_2	- Value of the conservative variable at point 2.

SetConservative() [3/3]

void CNumerics::SetConservative ( su2double *  val_u_0, su2double *  val_u_1, su2double *  val_u_2, su2double *  val_u_3  )

inline

Set the value of the conservative variables.

Parameters

[in]	val_u_0	- Value of the conservative variable at point 0.
[in]	val_u_1	- Value of the conservative variable at point 1.
[in]	val_u_2	- Value of the conservative variable at point 2.
[in]	val_u_3	- Value of the conservative variable at point 3.

SetConservative_ZeroOrder()

void CNumerics::SetConservative_ZeroOrder ( su2double *  val_u_i, su2double *  val_u_j  )

inline

Set the value of the conservative variables withour reconstruction.

Parameters

[in]	val_u_i	- Value of the conservative variable at point i.
[in]	val_u_j	- Value of the conservative variable at point j.

SetConsVarGradient() [1/4]

void CNumerics::SetConsVarGradient ( su2double **  val_consvar_grad_i, su2double **  val_consvar_grad_j  )

inline

Set the gradient of the conservative variables.

Parameters

[in]	val_consvar_grad_i	- Gradient of the conservative variable at point i.
[in]	val_consvar_grad_j	- Gradient of the conservative variable at point j.

SetConsVarGradient() [2/4]

void CNumerics::SetConsVarGradient ( su2double **  val_consvar_grad_0, su2double **  val_consvar_grad_1, su2double **  val_consvar_grad_2  )

inline

Set the gradient of the conservative variables.

Parameters

[in]	val_consvar_grad_0	- Gradient of the conservative variable at point 0.
[in]	val_consvar_grad_1	- Gradient of the conservative variable at point 1.
[in]	val_consvar_grad_2	- Gradient of the conservative variable at point 2.

SetConsVarGradient() [3/4]

void CNumerics::SetConsVarGradient ( su2double **  val_consvar_grad_0, su2double **  val_consvar_grad_1, su2double **  val_consvar_grad_2, su2double **  val_consvar_grad_3  )

inline

Set the gradient of the conservative variables.

Parameters

[in]	val_consvar_grad_0	- Gradient of the conservative variable at point 0.
[in]	val_consvar_grad_1	- Gradient of the conservative variable at point 1.
[in]	val_consvar_grad_2	- Gradient of the conservative variable at point 2.
[in]	val_consvar_grad_3	- Gradient of the conservative variable at point 3.

SetConsVarGradient() [4/4]

void CNumerics::SetConsVarGradient ( su2double **  val_consvar_grad )

inline

Set the gradient of the conservative variables.

Parameters

[in]

val_consvar_grad

- Gradient of the conservative variable which is a scalar.

SetCoord() [1/3]

void CNumerics::SetCoord ( su2double *  val_coord_i, su2double *  val_coord_j  )

inline

Set coordinates of the points.

Parameters

[in]	val_coord_i	- Coordinates of the point i.
[in]	val_coord_j	- Coordinates of the point j.

SetCoord() [2/3]

void CNumerics::SetCoord ( su2double *  val_coord_0, su2double *  val_coord_1, su2double *  val_coord_2  )

inline

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[in]	val_coord_0	- Coordinates of the point 0.
[in]	val_coord_1	- Coordinates of the point 1.
[in]	val_coord_2	- Coordinates of the point 2.

SetCoord() [3/3]

void CNumerics::SetCoord ( su2double *  val_coord_0, su2double *  val_coord_1, su2double *  val_coord_2, su2double *  val_coord_3  )

inline

This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.

Parameters

[in]	val_coord_0	- Coordinates of the point 0.
[in]	val_coord_1	- Coordinates of the point 1.
[in]	val_coord_2	- Coordinates of the point 2.
[in]	val_coord_3	- Coordinates of the point 3.

SetCrossDiff()

virtual void CNumerics::SetCrossDiff ( su2double  val_CDkw_i, su2double  val_CDkw_j  )

inlinevirtual

Set the value of the cross diffusion for the SST model.

Parameters

[in]	val_CDkw_i	- Value of the cross diffusion at point i.
[in]	val_CDkw_j	- Value of the cross diffusion at point j.

Reimplemented in CSourcePieceWise_TurbSST.

SetCrossProduction()

void CNumerics::SetCrossProduction ( su2double  val_crossproduction )

inlinevirtual

Residual for source term integration.

Parameters

[in]

val_crossproduction

- Value of the CrossProduction.

Reimplemented in CSourcePieceWise_TurbSA_Neg, and CSourcePieceWise_TurbSA.

SetDensity()

void CNumerics::SetDensity ( su2double  val_densityinc_i, su2double  val_densityinc_j  )

inline

Set the value of the density for the incompressible solver.

Parameters

[in]	val_densityinc_i	- Value of the pressure at point i.
[in]	val_densityinc_j	- Value of the pressure at point j.

SetDestruction()

void CNumerics::SetDestruction ( su2double  val_destruction )

inlinevirtual

Residual for source term integration.

Parameters

[in]

val_destruction

- Value of the Destruction.

Reimplemented in CSourcePieceWise_TurbSA_Neg, and CSourcePieceWise_TurbSA.

SetDiffusionCoeff()

void CNumerics::SetDiffusionCoeff ( su2double *  val_diffusioncoeff_i, su2double *  val_diffusioncoeff_j  )

inline

Set the diffusion coefficient.

Parameters

[in]	val_diffusioncoeff_i	- Value of the diffusion coefficients at i.
[in]	val_diffusioncoeff_j	- Value of the diffusion coefficients at j

SetDistance()

void CNumerics::SetDistance ( su2double  val_dist_i, su2double  val_dist_j  )

inline

Set the value of the distance from the nearest wall.

Parameters

[in]	val_dist_i	- Value of of the distance from point i to the nearest wall.
[in]	val_dist_j	- Value of of the distance from point j to the nearest wall.

SetdPdU()

void CNumerics::SetdPdU	(	su2double *	val_dPdU_i,
		su2double *	val_dPdU_j
	)

Sets the value of the derivative of pressure w.r.t. species density.

Parameters

[in]

iRho_s

SetdTdU()

void CNumerics::SetdTdU	(	su2double *	val_dTdU_i,
		su2double *	val_dTdU_j
	)

Sets the value of the derivative of temperature w.r.t. species density.

Parameters

[in]

iRho_s

SetdTvedU()

void CNumerics::SetdTvedU	(	su2double *	val_dTvedU_i,
		su2double *	val_dTvedU_j
	)

Sets the value of the derivative of vib-el. temperature w.r.t. species density.

Parameters

[in]

iRho_s

SetEddyViscosity()

void CNumerics::SetEddyViscosity ( su2double  val_eddy_viscosity_i, su2double  val_eddy_viscosity_j  )

inline

Set the eddy viscosity.

Parameters

[in]	val_eddy_viscosity_i	- Value of the eddy viscosity at point i.
[in]	val_eddy_viscosity_j	- Value of the eddy viscosity at point j.

SetEnthalpy()

void CNumerics::SetEnthalpy ( su2double  val_enthalpy_i, su2double  val_enthalpy_j  )

inline

Set the value of the enthalpy.

Parameters

[in]	val_enthalpy_i	- Value of the enthalpy at point i.
[in]	val_enthalpy_j	- Value of the enthalpy at point j.

SetF1blending()

virtual void CNumerics::SetF1blending ( su2double  val_F1_i, su2double  val_F1_j  )

inlinevirtual

Set the value of the first blending function.

Parameters

[in]	val_F1_i	- Value of the first Menter blending function at point i.
[in]	val_F1_j	- Value of the first Menter blending function at point j.

Reimplemented in CSourcePieceWise_TurbSST, CAvgGradCorrected_TurbSST, and CAvgGrad_TurbSST.

SetF2blending()

virtual void CNumerics::SetF2blending ( su2double  val_F1_i, su2double  val_F1_j  )

inlinevirtual

Set the value of the second blending function.

Parameters

[in]	val_F1_i	- Value of the second Menter blending function at point i.
[in]	val_F1_j	- Value of the second Menter blending function at point j.

Reimplemented in CSourcePieceWise_TurbSST.

SetGridVel()

void CNumerics::SetGridVel ( su2double *  val_gridvel_i, su2double *  val_gridvel_j  )

inline

Set the velocity of the computational grid.

Parameters

[in]	val_gridvel_i	- Grid velocity of the point i.
[in]	val_gridvel_j	- Grid velocity of the point j.

SetHIndex()

void CNumerics::SetHIndex

(

unsigned short

val_Index

)

Retrieves the value of the species density in the primitive variable vector.

Parameters

[in]

iRho_s

SetJacobian_Axisymmetric()

void CNumerics::SetJacobian_Axisymmetric ( su2double **  val_Jacobian_i, CConfig *  config  )

inlinevirtual

Calculation of axisymmetric source term Jacobian.

Parameters

[out]	val_Jacobian_i	- Jacobian of the numerical method at node i (implicit computation).
[in]	config	- Definition of the particular problem.

SetLambda()

void CNumerics::SetLambda ( su2double  val_lambda_i, su2double  val_lambda_j  )

inline

Set the value of the spectral radius.

Parameters

[in]	val_lambda_i	- Value of the spectral radius at point i.
[in]	val_lambda_j	- Value of the spectral radius at point j.

SetLaminarViscosity()

void CNumerics::SetLaminarViscosity ( su2double  val_laminar_viscosity_i, su2double  val_laminar_viscosity_j  )

inline

Set the laminar viscosity.

Parameters

[in]	val_laminar_viscosity_i	- Value of the laminar viscosity at point i.
[in]	val_laminar_viscosity_j	- Value of the laminar viscosity at point j.

SetNeighbor()

void CNumerics::SetNeighbor ( unsigned short  val_neighbor_i, unsigned short  val_neighbor_j  )

inline

Set the number of neighbor to a point.

Parameters

[in]	val_neighbor_i	- Number of neighbor to point i.
[in]	val_neighbor_j	- Number of neighbor to point j.

SetNormal()

void CNumerics::SetNormal ( su2double *  val_normal )

inline

Set the value of the normal vector to the face between two points.

Parameters

[in]

val_normal

- Normal vector, the norm of the vector is the area of the face.

SetPastSol()

void CNumerics::SetPastSol	(	su2double *	val_u_nM1,
		su2double *	val_u_n,
		su2double *	val_u_nP1
	)

Set the solution at different times.

Parameters

[in]	val_u_nM1	Conservative solution at time n-1.
[in]	val_u_n	Conservative solution at time n.
[in]	val_u_nP1	Conservative solution at time n+1.

SetPastVolume()

void CNumerics::SetPastVolume	(	su2double	val_volume_nM1,
		su2double	val_volume_n,
		su2double	val_volume_nP1
	)

Set the control volume at different times.

Parameters

[in]	val_volume_nM1	- Control volume at time n-1.
[in]	val_volume_n	- Control volume at time n.
[in]	val_volume_nP1	- Control volume at time n+1.

SetPIndex()

void CNumerics::SetPIndex

(

unsigned short

val_Index

)

Retrieves the value of the species density in the primitive variable vector.

Parameters

[in]

iRho_s

SetPressure()

void CNumerics::SetPressure ( su2double  val_pressure_i, su2double  val_pressure_j  )

inline

Set the value of the pressure.

Parameters

[in]	val_pressure_i	- Value of the pressure at point i.
[in]	val_pressure_j	- Value of the pressure at point j.

SetPrimitive()

void CNumerics::SetPrimitive ( su2double *  val_v_i, su2double *  val_v_j  )

inline

Set the value of the primitive variables.

Parameters

[in]	val_v_i	- Value of the primitive variable at point i.
[in]	val_v_j	- Value of the primitive variable at point j.

SetPrimVarGradient()

void CNumerics::SetPrimVarGradient ( su2double **  val_primvar_grad_i, su2double **  val_primvar_grad_j  )

inline

Set the gradient of the primitive variables.

Parameters

[in]	val_primvar_grad_i	- Gradient of the primitive variable at point i.
[in]	val_primvar_grad_j	- Gradient of the primitive variable at point j.

SetPrimVarLimiter()

void CNumerics::SetPrimVarLimiter ( su2double *  val_primvar_lim_i, su2double *  val_primvar_lim_j  )

inline

Set the Limiter of the primitive variables.

Parameters

[in]	val_primvar_lim_i	- Limiter of the primitive variable at point i.
[in]	val_primvar_lim_j	- Limiter of the primitive variable at point j.

SetProduction()

void CNumerics::SetProduction ( su2double  val_production )

inlinevirtual

Residual for source term integration.

Parameters

[in]

val_production

- Value of the Production.

Reimplemented in CSourcePieceWise_TurbSA_Neg, and CSourcePieceWise_TurbSA.

SetRhoCvtrIndex()

void CNumerics::SetRhoCvtrIndex

(

unsigned short

val_Index

)

Retrieves the value of the species density in the primitive variable vector.

Parameters

[in]

iRho_s

SetRhoCvveIndex()

void CNumerics::SetRhoCvveIndex

(

unsigned short

val_Index

)

Retrieves the value of the species density in the primitive variable vector.

Parameters

[in]

iRho_s

SetRhoIndex()

void CNumerics::SetRhoIndex

(

unsigned short

val_Index

)

Retrieves the value of the species density in the primitive variable vector.

Parameters

[in]

iRho_s

SetRhosIndex()

void CNumerics::SetRhosIndex

(

unsigned short

val_Index

)

Retrieves the value of the species density in the primitive variable vector.

Parameters

[in]

iRho_s

SetSecondary()

void CNumerics::SetSecondary ( su2double *  val_s_i, su2double *  val_s_j  )

inline

Set the value of the primitive variables.

Parameters

[in]	val_v_i	- Value of the primitive variable at point i.
[in]	val_v_j	- Value of the primitive variable at point j.

SetSensor()

void CNumerics::SetSensor ( su2double  val_sensor_i, su2double  val_sensor_j  )

inline

Set the value of the pressure sensor.

Parameters

[in]	val_sensor_i	Pressure sensor at point i.
[in]	val_sensor_j	Pressure sensor at point j.

SetSoundSpeed()

void CNumerics::SetSoundSpeed ( su2double  val_soundspeed_i, su2double  val_soundspeed_j  )

inline

Set the value of the sound speed.

Parameters

[in]	val_soundspeed_i	- Value of the sound speed at point i.
[in]	val_soundspeed_j	- Value of the sound speed at point j.

SetStrainMag()

void CNumerics::SetStrainMag ( su2double  val_strainmag_i, su2double  val_strainmag_j  )

inline

Set the value of the rate of strain magnitude.

Parameters

[in]	val_StrainMag_i	- Value of the magnitude of rate of strain at point i.
[in]	val_StrainMag_j	- Value of the magnitude of rate of strain at point j.

SetTemperature()

void CNumerics::SetTemperature ( su2double  val_temp_i, su2double  val_temp_j  )

inline

Set the value of the temperature.

Parameters

[in]	val_temp_i	- Value of the temperature at point i.
[in]	val_temp_j	- Value of the temperature at point j.

SetThermalConductivity()

void CNumerics::SetThermalConductivity ( su2double  val_thermal_conductivity_i, su2double  val_thermal_conductivity_j  )

inline

Set the thermal conductivity (translational/rotational)

Parameters

[in]	val_thermal_conductivity_i	- Value of the thermal conductivity at point i.
[in]	val_thermal_conductivity_j	- Value of the thermal conductivity at point j.
[in]	iSpecies	- Value of the species.

SetThermalConductivity_ve()

void CNumerics::SetThermalConductivity_ve ( su2double  val_thermal_conductivity_ve_i, su2double  val_thermal_conductivity_ve_j  )

inline

Set the thermal conductivity (translational/rotational)

Parameters

[in]	val_thermal_conductivity_i	- Value of the thermal conductivity at point i.
[in]	val_thermal_conductivity_j	- Value of the thermal conductivity at point j.
[in]	iSpecies	- Value of the species.

SetTimeStep()

void CNumerics::SetTimeStep ( su2double  val_timestep )

inline

Set the time step.

Parameters

[in]

val_timestep

- Value of the time step.

SetTIndex()

void CNumerics::SetTIndex

(

unsigned short

val_Index

)

Retrieves the value of the species density in the primitive variable vector.

Parameters

[in]

iRho_s

SetTransVar()

void CNumerics::SetTransVar ( su2double *  val_transvar_i, su2double *  val_transvar_j  )

inline

Set the value of the turbulent variable.

Parameters

[in]	val_transvar_i	- Value of the turbulent variable at point i.
[in]	val_transvar_j	- Value of the turbulent variable at point j.

SetTransVarGradient()

void CNumerics::SetTransVarGradient ( su2double **  val_transvar_grad_i, su2double **  val_transvar_grad_j  )

inline

Set the gradient of the turbulent variables.

Parameters

[in]	val_turbvar_grad_i	- Gradient of the turbulent variable at point i.
[in]	val_turbvar_grad_j	- Gradient of the turbulent variable at point j.

SetTurbAdjointGradient()

void CNumerics::SetTurbAdjointGradient ( su2double **  val_turbpsivar_grad_i, su2double **  val_turbpsivar_grad_j  )

inline

Set the gradient of the adjoint turbulent variables.

Parameters

[in]	val_turbpsivar_grad_i	- Gradient of the adjoint turbulent variable at point i.
[in]	val_turbpsivar_grad_j	- Gradient of the adjoint turbulent variable at point j.

SetTurbAdjointVar()

void CNumerics::SetTurbAdjointVar ( su2double *  val_turbpsivar_i, su2double *  val_turbpsivar_j  )

inline

Set the value of the adjoint turbulent variable.

Parameters

[in]	val_turbpsivar_i	- Value of the adjoint turbulent variable at point i.
[in]	val_turbpsivar_j	- Value of the adjoint turbulent variable at point j.

SetTurbKineticEnergy()

void CNumerics::SetTurbKineticEnergy ( su2double  val_turb_ke_i, su2double  val_turb_ke_j  )

inline

Set the turbulent kinetic energy.

Parameters

[in]	val_turb_ke_i	- Value of the turbulent kinetic energy at point i.
[in]	val_turb_ke_j	- Value of the turbulent kinetic energy at point j.

SetTurbVar()

void CNumerics::SetTurbVar ( su2double *  val_turbvar_i, su2double *  val_turbvar_j  )

inline

Set the value of the turbulent variable.

Parameters

[in]	val_turbvar_i	- Value of the turbulent variable at point i.
[in]	val_turbvar_j	- Value of the turbulent variable at point j.

SetTurbVarGradient()

void CNumerics::SetTurbVarGradient ( su2double **  val_turbvar_grad_i, su2double **  val_turbvar_grad_j  )

inline

Set the gradient of the turbulent variables.

Parameters

[in]	val_turbvar_grad_i	- Gradient of the turbulent variable at point i.
[in]	val_turbvar_grad_j	- Gradient of the turbulent variable at point j.

SetTveIndex()

void CNumerics::SetTveIndex

(

unsigned short

val_Index

)

Retrieves the value of the species density in the primitive variable vector.

Parameters

[in]

iRho_s

SetUndivided_Laplacian()

void CNumerics::SetUndivided_Laplacian ( su2double *  val_und_lapl_i, su2double *  val_und_lapl_j  )

inline

Set the value of undivided laplacian.

Parameters

[in]	val_und_lapl_i	Undivided laplacian at point i.
[in]	val_und_lapl_j	Undivided laplacian at point j.

SetVelIndex()

void CNumerics::SetVelIndex

(

unsigned short

val_Index

)

Retrieves the value of the velocity index in the primitive variable vector.

Parameters

[in]

i(rho*u)

SetVelocity2_Inf()

void CNumerics::SetVelocity2_Inf ( su2double  val_velocity2 )

inline

Set the freestream velocity square.

Parameters

[in]

SetVelocity2_Inf

- Value of the square of the freestream velocity.

SetVolume()

void CNumerics::SetVolume ( su2double  val_volume )

inline

Set the value of the volume of the control volume.

Parameters

[in]

val_volume

Volume of the control volume.

SetVorticity()

void CNumerics::SetVorticity ( su2double *  val_vorticity_i, su2double *  val_vorticity_j  )

inline

Set the value of the vorticity.

Parameters

[in]

val_vorticity

- Value of the vorticity.

SetWindGust()

void CNumerics::SetWindGust ( su2double *  val_windgust_i, su2double *  val_windgust_j  )

inline

Set the wind gust value.

Parameters

[in]	val_windgust_i	- Wind gust of the point i.
[in]	val_windgust_j	- Wind gust of the point j.

SetWindGustDer()

void CNumerics::SetWindGustDer ( su2double *  val_windgustder_i, su2double *  val_windgustder_j  )

inline

Set the wind gust derivatives values.

Parameters

[in]	val_windgust_i	- Wind gust derivatives of the point i.
[in]	val_windgust_j	- Wind gust derivatives of the point j.

---

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_structure.cpp