MeltPoolDG::CompressibleFlow Namespace Reference

This file contains various functions that can be used to set and evaluate boundary conditions for the compressible flow solver. The functions can be directly used with the BoundaryConditions class, which provides an interface to manage and evaluate the different boundary conditions in the solver. More...

Namespaces
namespace	EOS

Classes
class	BoundaryConditions
	Helper class taking care of all boundary condition related computations for the compressible flow solver. More...
struct	CombinedInflowNoSlipWallValueInterpretation
struct	ConcreteConvectiveFluxImpl
struct	ConcreteConvectiveFluxImpl< dim, 1, number, Value, Flux >
struct	ConcreteDiffusiveFluxImpl
struct	ConcreteDiffusiveFluxImpl< dim, 1, number, Value, Gradient, Flux >
struct	ConcreteDofStateViewImpl
struct	ConcreteDofStateViewImpl< dim, 1, number, StateType >
struct	ConcreteDofValueAndGradientStateViewImpl
struct	ConcreteDofValueAndGradientStateViewImpl< dim, 1, number, Value, Gradient >
struct	ConcreteDofValueViewImpl
struct	ConcreteDofValueViewImpl< dim, 1, StateType >
struct	ConcreteFluxViewImpl
struct	ConcreteFluxViewImpl< dim, 1, FluxType >
class	ConservativeVariablesFunction
struct	ConservedVariableIndex
class	ConservedVariablesPostProcessor
struct	ConvectiveFlux
struct	ConvectiveKernels
	Convective kernel operations for compressible flow solvers. More...
class	CutDGOperation
	Operation that performs a full time step for the compressible single-phase Navier-Stokes equations in a cutDG context. More...
class	CutDGOperator
	Operator for the matrix-free evaluation of a compressible single-phase flow cutDG formulation. More...
struct	CutSolverData
	Collection of cut-related solver parameters required by the cut single-phase and multiphase compressible Navier-Stokes operators. More...
class	DGOperation
	Operation that performs a full time step for the compressible Navier-Stokes. More...
class	DGOperatorBase
	Interface of the compressible flow operator interacting with the compressible flow operation. More...
class	DGOperatorExplicit
	Operator for the matrix-free evaluation of a compressible single-phase flow cutDG formulation for explicit time integration. More...
class	DGOperatorImplicit
	Operator for the matrix-free evaluation of a compressible single-phase flow cutDG formulation for implicit time integration. More...
class	DGOperatorImplicitExplicit
	Operator for the matrix-free evaluation of a compressible single-phase flow cutDG formulation for implicit-explicit time integration. More...
struct	DiffusiveFlux
struct	DofGradientMixin
struct	DofGradientView
struct	DofStateView
struct	DofValueAndGradientStateView
struct	DofValueMixin
struct	DofValueView
struct	EOSData
	Collection of parameters related to the equation of state for a compressible or nearly incompressible fluid. More...
struct	ExternalFlowForce
	An abstract interface for defining external forces acting on the fluid that must be evaluated and incorporated during the cell loop of an explicit time integration scheme. More...
struct	ExternalFlowForceJacobian
struct	FluxMixin
struct	FluxView
class	FreeJetInflow
class	FreeJetVelocityFunction
	Enum for the type of velocity profile of a free jet inflow. More...
struct	InflowValueInterpretation
struct	InputDefinedBoundaryCondition
struct	InputDefinedFreeJetInflow
struct	InputDefinedInitialCondition
struct	InputDefinedSubdividedHyperRectangleDomain
class	Material
	A class which provides all relevant material properties for a specific phase. More...
struct	MaterialMixin
struct	MaterialPhaseData
	Collection of material parameters for a specific fluid phase. More...
struct	MaterialSpeciesData
	Collection of material parameters for a specific species. More...
class	MaterialVariablesPostProcessor
struct	MaterialView
struct	MultiphaseOperationScratchData
	Scratch data structure for compressible multiphase flow solvers. More...
struct	MultiSpeciesDofStateView
struct	MultiSpeciesDofValueAndGradientStateView
struct	MultiSpeciesDofValueView
struct	MultiSpeciesFluxView
struct	MultiSpeciesMaterialMixin
struct	OperationData
	Collection of parameters required by the compressible Navier-Stokes operator. More...
struct	OperationScratchData
	Scratch data structure for compressible single-phase flow solvers. More...
class	OperationTypeErasure
	Common interface class for compressible flow operation classes based on the type erasure idiom. More...
struct	OutputManager
class	PrimitiveVariablesPostProcessor
struct	SpeciesTransportConvectiveFlux
struct	SpeciesTransportDiffusiveFlux
struct	ViscousKernels
	Viscous kernel operations for compressible flow solvers. More...

Concepts
concept	IsConservedStateCompatible
concept	IsConservedGradientCompatible
concept	IsConservedView
concept	IsPrimitiveView
concept	IsMaterialView
concept	IsValueView
concept	IsGradientView
concept	IsFluxKernel
concept	CellEvaluatorType
	Concept to check whether a given type conforms to a valid cell evaluator interface.
concept	FaceEvaluatorType
	Concept to check whether a given type conforms to a valid face evaluator interface.

Typedefs
template<int dim, typename number , int n_species = 1, typename VectorizedArrayType = dealii::VectorizedArray<number>>
using	ConservedVariablesType = dealii::Tensor< 1, n_conserved_variables< dim, n_species >, VectorizedArrayType >
template<int dim, typename number , int n_species = 1, typename VectorizedArrayType = dealii::VectorizedArray<number>>
using	ConservedVariablesGradientType = dealii::Tensor< 1, n_conserved_variables< dim, n_species >, dealii::Tensor< 1, dim, VectorizedArrayType > >
template<int dim, typename number , int n_species = 1>
using	FluxType = dealii::Tensor< 1, n_conserved_variables< dim, n_species >, dealii::Tensor< 1, dim, dealii::VectorizedArray< number > > >
template<int dim, typename number , int n_species = 1>
using	FaceFluxType = dealii::Tensor< 1, n_conserved_variables< dim, n_species >, dealii::VectorizedArray< number > >
template<int dim, typename number , int n_species = 1>
using	FaceGradientFluxType = dealii::Tensor< 1, n_conserved_variables< dim, n_species >, dealii::Tensor< 1, dim, dealii::VectorizedArray< number > > >
template<int dim, typename number , int n_species = 1>
using	SourceType = dealii::Tensor< 1, n_conserved_variables< dim, n_species >, dealii::VectorizedArray< number > >
template<int dim, int n_species, typename number , typename Value , typename Flux >
using	NSpeciesConvectiveFlux = typename ConcreteConvectiveFluxImpl< dim, n_species, number, Value, Flux >::type
template<int dim, int n_species, typename number , typename Value , typename Gradient , typename Flux >
using	NSpeciesDiffusiveFlux = typename ConcreteDiffusiveFluxImpl< dim, n_species, number, Value, Gradient, Flux >::type
template<int dim, int n_species, IsConservedStateCompatible< dim > StateType>
using	NSpeciesDofValueView = typename ConcreteDofValueViewImpl< dim, n_species, StateType >::type
template<int dim, int n_species, typename number , IsConservedStateCompatible< dim > StateType>
using	NSpeciesDofStateView = typename ConcreteDofStateViewImpl< dim, n_species, number, StateType >::type
template<int dim, int n_species, typename number , IsConservedStateCompatible< dim > Value, IsConservedGradientCompatible< dim > Gradient>
using	NSpeciesDofValueAndGradientStateView = typename ConcreteDofValueAndGradientStateViewImpl< dim, n_species, number, Value, Gradient >::type
template<int dim, int n_species, typename FluxType >
using	NSpeciesFluxView = typename ConcreteFluxViewImpl< dim, n_species, FluxType >::type

Functions
	BETTER_ENUM (RampUpType, char, none, linear, exponential, cosine)
	Enum for the type of ramp up function used for the velocity at an inflow boundary.
	BETTER_ENUM (BoundaryConditionType, char, combined_inflow_no_slip_wall, inflow, slip_wall, no_slip_wall, subsonic_outflow_fixed_energy, subsonic_outflow_fixed_pressure)
template<int dim, typename number >
void	add_hyper_rectangle_custom_boundary_condition_parameters (dealii::ParameterHandler &prm, std::array< InputDefinedBoundaryCondition< dim, number >, 2 *dim > &boundary_conditions)
template<int dim, typename number , CellEvaluatorType< dim, dim+2, number, dealii::VectorizedArray< number > > Integrator, bool is_viscous = true>
DEAL_II_ALWAYS_INLINE std::tuple< ConservedVariablesType< dim, number >, ConservedVariablesGradientType< dim, number > >	rhs_cell_integral_kernel (const Integrator &evaluator, const unsigned int q, const dealii::Tensor< 1, dim, dealii::VectorizedArray< number > > *constant_body_force, const ConvectiveKernels< dim, number > &convective_terms, const ViscousKernels< dim, number > &viscous_terms, const std::unique_ptr< dealii::Function< dim > > &body_force)
	Computes the right-hand side cell integral kernels at a quadrature point.
template<int dim, typename number , FaceEvaluatorType< dim, dim+2, number, dealii::VectorizedArray< number > > Integrator, bool is_viscous = true>
DEAL_II_ALWAYS_INLINE std::tuple< ConservedVariablesType< dim, number >, ConservedVariablesType< dim, number >, ConservedVariablesGradientType< dim, number >, ConservedVariablesGradientType< dim, number > >	rhs_face_integral_kernel (const Integrator &evaluator_m, const Integrator &evaluator_p, const unsigned int q, dealii::VectorizedArray< number > penalty_parameter, const ConvectiveKernels< dim, number > &convective_terms, const ViscousKernels< dim, number > &viscous_terms)
	Computes the right-hand side face integral kernels at a face quadrature point.
template<int dim, typename number , FaceEvaluatorType< dim, dim+2, number, dealii::VectorizedArray< number > > Integrator, bool is_viscous = true, bool is_gas_phase = true>
DEAL_II_ALWAYS_INLINE std::tuple< ConservedVariablesType< dim, number >, ConservedVariablesGradientType< dim, number > >	rhs_boundary_face_integral_kernel (const Integrator &evaluator_m, const unsigned int q, const dealii::types::boundary_id boundary_id, const dealii::VectorizedArray< number > penalty_parameter, const ConvectiveKernels< dim, number > &convective_terms, const ViscousKernels< dim, number > &viscous_terms, const Material< dim, number > &material, const BoundaryConditions< dim, number > &boundary_conditions)
	Computes the right-hand side boundary face integral kernels at a boundary face quadrature point.
template<int dim, typename ConservedVariablesView , typename WritableFluxView >
DEAL_II_ALWAYS_INLINE void	convective_flux (const ConservedVariablesView &conserved_variables, const WritableFluxView &flux)
template<int dim, typename number >
DEAL_II_ALWAYS_INLINE dealii::Tensor< 1, dim, dealii::Tensor< 1, dim, dealii::VectorizedArray< number > > >	viscous_stress_tensor (const dealii::Tensor< 1, dim, dealii::Tensor< 1, dim, dealii::VectorizedArray< number > > > &grad_velocity, const dealii::VectorizedArray< number > dynamic_viscosity)
template<int dim, typename VectorizedArrayType , typename DofStateView , typename WritableFluxView >
DEAL_II_ALWAYS_INLINE void	diffusive_flux (const DofStateView &conserved_variables, const WritableFluxView &flux)
	BETTER_ENUM (NumericalFluxType, char, lax_friedrichs_modified, lax_friedrichs_exact, harten_lax_vanleer) BETTER_ENUM(LinearizedConvectiveFluxJumpType
	BETTER_ENUM (JacobianType, char, exact, finite_difference)
	BETTER_ENUM (OutputType, char, conserved_variables, primitive_variables, material_quantities)
	BETTER_ENUM (Idx1D, char, density, momentum_x, energy)
	Index sets for the components of the compressible Navier-Stokes equations.
	BETTER_ENUM (Idx2D, char, density, momentum_x, momentum_y, energy)
	BETTER_ENUM (Idx3D, char, density, momentum_x, momentum_y, momentum_z, energy)
template<int dim, typename number >
DEAL_II_ALWAYS_INLINE dealii::Tensor< 1, dim, dealii::VectorizedArray< number > >	calculate_velocity (const ConservedVariablesType< dim, number > &conserved_variables)
	Calculate the velocity from the conserved variables by computing u = (ρu)/ρ.
template<int dim, typename number >
DEAL_II_ALWAYS_INLINE dealii::Tensor< 2, dim, dealii::VectorizedArray< number > >	calculate_grad_velocity (const ConservedVariablesType< dim, number > &conserved_variables, const ConservedVariablesGradientType< dim, number > &grad_conserved_variables)
	Calculate the velocity gradient.
template<int dim, typename Number >
void	calculate_penalty_parameter (dealii::AlignedVector< dealii::VectorizedArray< Number > > &array_penalty_parameter, const dealii::MatrixFree< dim, Number > &matrix_free, const std::string &domain_representation_type, const unsigned int dof_index=0, const Number scaling_factor=1.0)
	This function computes the local values of the internal penalty parameter used in the viscous numerical flux.
template<int dim, typename number >
void	update_primitive_variables_solution (dealii::LinearAlgebra::distributed::Vector< number > &solution_primitive_variables, const dealii::LinearAlgebra::distributed::Vector< number > &solution, const ScratchData< dim, dim, number > &scratch_data, const unsigned int dof_idx, const unsigned int quad_idx, const Material< dim, number > *material_liquid, const Material< dim, number > *material_gas=nullptr)
	Update the primitive variable solution according to the current solution vector.
template<typename DofViewType , typename VectorizedArrayType >
DEAL_II_ALWAYS_INLINE VectorizedArrayType	maximum_local_wave_speed (const DofViewType &u_m, const DofViewType &u_p)

Variables
template<int dim, int n_species = 1>
constexpr unsigned int	n_conserved_variables = dim + 2 + (n_species - 1)
	char
	analytic
	lambda_fd
	complete_fd

Detailed Description

This file contains various functions that can be used to set and evaluate boundary conditions for the compressible flow solver. The functions can be directly used with the BoundaryConditions class, which provides an interface to manage and evaluate the different boundary conditions in the solver.

Type definitions and helper functions for the compressible flow implementations.

A collection of helper functions that might be useful when solving the compressible Navier-Stokes equations with an explicit time stepping strategy.

This operation solves the compressible Navier-Stokes equations, comprising the primary variables.

This operator solves the compressible Navier-Stokes equations, comprising the primary variables.

Collection of convective term computations for the compressible Navier-Stokes equations.

• density (ρ)
• momentum (ρ u)
• volume-specific energy (ρ E) using the cutDG method for single-phase problems.

It is an extension of deal.II step-67 and is based on

Fehn, N., Wall, W. A., & Kronbichler, M. (2019). A matrix‐free high‐order discontinuous Galerkin compressible Navier‐Stokes solver: A performance comparison of compressible and incompressible formulations for turbulent incompressible flows. International Journal for Numerical Methods in Fluids, 89(3), 71-102.

and

Ritthaler, A. (2024). A matrix-free cutDG formulation for complex flows, Master's Thesis.

• density (ρ)
• momentum (ρ u)
• volume-specific energy (ρ E)

It is an extension of deal.II step-67 and is based on the paper

Fehn, N., Wall, W. A., & Kronbichler, M. (2019). A matrix‐free high‐order discontinuous Galerkin compressible Navier‐Stokes solver: A performance comparison of compressible and incompressible formulations for turbulent incompressible flows. International Journal for Numerical Methods in Fluids, 89(3), 71-102.

This file contains type aliases for the kernels used in the multi- and single-species compressible flow solver. The main purpose is that the type aliases automatically resolve to the correct kernel type depending on the number of species in the simulation. For example, for single-species simulations, the kernels resolve to the standard ConvectiveFlux and DiffusiveFlux, while for multi-species simulations, they resolve to the corresponding SpeciesTransportConvectiveFlux and SpeciesTransportDiffusiveFlux.

This file contains type aliases for the state views used in the multi- and single-species compressible flow solver. The main purpose is that the type aliases automatically resolve to the correct state view type depending on the number of species in the simulation. For example, for single-species simulations, the state views resolve to the standard DofStateView and DofValueAndGradientStateView, while for multi-species simulations, they resolve to the corresponding MultiSpeciesDofStateView and MultiSpeciesDofValueAndGradientStateView.

Typedef Documentation

ConservedVariablesGradientType

template<int dim, typename number , int n_species = 1, typename VectorizedArrayType = dealii::VectorizedArray<number>>

using MeltPoolDG::CompressibleFlow::ConservedVariablesGradientType = typedef dealii:: Tensor<1, n_conserved_variables<dim, n_species>, dealii::Tensor<1, dim, VectorizedArrayType> >

Type alias for the gradient of the conserved variables in the compressible flow solver given at a vectorized set of coordinates.

ConservedVariablesType

template<int dim, typename number , int n_species = 1, typename VectorizedArrayType = dealii::VectorizedArray<number>>

using MeltPoolDG::CompressibleFlow::ConservedVariablesType = typedef dealii::Tensor<1, n_conserved_variables<dim, n_species>, VectorizedArrayType>

Type alias for the conserved variables in the compressible flow solver given at a vectorized set of coordinates.

FaceFluxType

template<int dim, typename number , int n_species = 1>

using MeltPoolDG::CompressibleFlow::FaceFluxType = typedef dealii::Tensor<1, n_conserved_variables<dim, n_species>, dealii::VectorizedArray<number> >

Type alias for the fluxes at faces in the compressible flow solver given at a vectorized set of coordinates (contracted with normal vector). This includes both convective and diffusive fluxes.

FaceGradientFluxType

template<int dim, typename number , int n_species = 1>

using MeltPoolDG::CompressibleFlow::FaceGradientFluxType = typedef dealii::Tensor<1, n_conserved_variables<dim, n_species>, dealii::Tensor<1, dim, dealii::VectorizedArray<number> >>

FluxType

template<int dim, typename number , int n_species = 1>

using MeltPoolDG::CompressibleFlow::FluxType = typedef dealii::Tensor<1, n_conserved_variables<dim, n_species>, dealii::Tensor<1, dim, dealii::VectorizedArray<number> >>

Type alias for the fluxes in the compressible flow solver given at a vectorized set of coordinates. This includes both convective and diffusive fluxes.

NSpeciesConvectiveFlux

template<int dim, int n_species, typename number , typename Value , typename Flux >

using MeltPoolDG::CompressibleFlow::NSpeciesConvectiveFlux = typedef typename ConcreteConvectiveFluxImpl<dim, n_species, number, Value, Flux>::type

Type alias for the ConvectiveFlux for a specific number of species. This alias resolves to the appropriate kernel type depending on the number of species in the simulation.

NSpeciesDiffusiveFlux

template<int dim, int n_species, typename number , typename Value , typename Gradient , typename Flux >

using MeltPoolDG::CompressibleFlow::NSpeciesDiffusiveFlux = typedef typename ConcreteDiffusiveFluxImpl<dim, n_species, number, Value, Gradient, Flux>::type

Type alias for the DiffusiveFlux for a specific number of species. This alias resolves to the appropriate kernel type depending on the number of species in the simulation.

NSpeciesDofStateView

template<int dim, int n_species, typename number , IsConservedStateCompatible< dim > StateType>

using MeltPoolDG::CompressibleFlow::NSpeciesDofStateView = typedef typename ConcreteDofStateViewImpl<dim, n_species, number, StateType>::type

Type alias for the DofStateView for a specific number of species. This alias resolves to the appropriate state view type depending on the number of species in the simulation.

NSpeciesDofValueAndGradientStateView

template<int dim, int n_species, typename number , IsConservedStateCompatible< dim > Value, IsConservedGradientCompatible< dim > Gradient>

using MeltPoolDG::CompressibleFlow::NSpeciesDofValueAndGradientStateView = typedef typename ConcreteDofValueAndGradientStateViewImpl<dim, n_species, number, Value, Gradient>:: type

Type alias for the DofValueAndGradientStateView for a specific number of species. This alias resolves to the appropriate state view type depending on the number of species in the simulation.

NSpeciesDofValueView

template<int dim, int n_species, IsConservedStateCompatible< dim > StateType>

using MeltPoolDG::CompressibleFlow::NSpeciesDofValueView = typedef typename ConcreteDofValueViewImpl<dim, n_species, StateType>::type

Type alias for the DofValueView for a specific number of species. This alias resolves to the appropriate state view type depending on the number of species in the simulation.

NSpeciesFluxView

template<int dim, int n_species, typename FluxType >

using MeltPoolDG::CompressibleFlow::NSpeciesFluxView = typedef typename ConcreteFluxViewImpl<dim, n_species, FluxType>::type

Type alias for the FluxView for a specific number of species. This alias resolves to the appropriate flux view type depending on the number of species in the simulation.

SourceType

template<int dim, typename number , int n_species = 1>

using MeltPoolDG::CompressibleFlow::SourceType = typedef dealii::Tensor<1, n_conserved_variables<dim, n_species>, dealii::VectorizedArray<number> >

Type alias for source terms in the compressible flow solver given at a vectorized set of coordinates.

Function Documentation

add_hyper_rectangle_custom_boundary_condition_parameters()

template<int dim, typename number >

void MeltPoolDG::CompressibleFlow::add_hyper_rectangle_custom_boundary_condition_parameters	(	dealii::ParameterHandler &	prm,
		std::array< InputDefinedBoundaryCondition< dim, number >, 2 *dim > &	boundary_conditions
	)

For a hyper-rectangular domain, this function adds the boundary condition parameters for all boundaries to the parameter handler. For this at each boundary the corresponding function of the boundary conditions object is called, which reads the parameters from the user input file and stores them in the corresponding boundary condition struct. The ordering in the passed array is the same as the boundary id provided by deal.II, i.e., for a 2D domain, the first two entries correspond to the boundaries with normal in x-direction (boundary ids 0 and 1), and the second two entries correspond to the boundaries with normal in y-direction (boundary ids 2 and 3). Subsequently, for 3D domains, the last two entries correspond to the boundaries with normal in z-direction (boundary ids 4 and 5).

Parameters

prm	Parameter handler to which the parameters will be added.
boundary_conditions	Array of boundary condition structs for all boundaries of the domain.

BETTER_ENUM() [1/8]

MeltPoolDG::CompressibleFlow::BETTER_ENUM	(	BoundaryConditionType	,
		char	,
		combined_inflow_no_slip_wall	,
		inflow	,
		slip_wall	,
		no_slip_wall	,
		subsonic_outflow_fixed_energy	,
		subsonic_outflow_fixed_pressure
	)

An enum for the various boundary conditions supported by the compressible flow solver.

BETTER_ENUM() [2/8]

MeltPoolDG::CompressibleFlow::BETTER_ENUM	(	Idx1D	,
		char	,
		density	,
		momentum_x	,
		energy
	)

Index sets for the components of the compressible Navier-Stokes equations.

BETTER_ENUM() [3/8]

MeltPoolDG::CompressibleFlow::BETTER_ENUM	(	Idx2D	,
		char	,
		density	,
		momentum_x	,
		momentum_y	,
		energy
	)

BETTER_ENUM() [4/8]

MeltPoolDG::CompressibleFlow::BETTER_ENUM	(	Idx3D	,
		char	,
		density	,
		momentum_x	,
		momentum_y	,
		momentum_z	,
		energy
	)

BETTER_ENUM() [5/8]

MeltPoolDG::CompressibleFlow::BETTER_ENUM	(	JacobianType	,
		char	,
		exact	,
		finite_difference
	)

BETTER_ENUM() [6/8]

MeltPoolDG::CompressibleFlow::BETTER_ENUM	(	NumericalFluxType	,
		char	,
		lax_friedrichs_modified	,
		lax_friedrichs_exact	,
		harten_lax_vanleer
	)

BETTER_ENUM() [7/8]

MeltPoolDG::CompressibleFlow::BETTER_ENUM	(	OutputType	,
		char	,
		conserved_variables	,
		primitive_variables	,
		material_quantities
	)

BETTER_ENUM() [8/8]

MeltPoolDG::CompressibleFlow::BETTER_ENUM	(	RampUpType	,
		char	,
		none	,
		linear	,
		exponential	,
		cosine
	)

Enum for the type of ramp up function used for the velocity at an inflow boundary.

calculate_grad_velocity()

template<int dim, typename number >

DEAL_II_ALWAYS_INLINE dealii::Tensor< 2, dim, dealii::VectorizedArray< number > > MeltPoolDG::CompressibleFlow::calculate_grad_velocity ( const ConservedVariablesType< dim, number > &  conserved_variables, const ConservedVariablesGradientType< dim, number > &  grad_conserved_variables  )

inline

Calculate the velocity gradient.

Calculate the gradient of the velocity from the conserved variables and their gradients by computing grad(u) = 1/ρ * (grad(ρu) - u*grad(ρ)).

Parameters

conserved_variables	Current values of the conserved variables.
grad_conserved_variables	Current gradient of the conserved variables.

Returns

Current gradient of the velocity.

calculate_penalty_parameter()

template<int dim, typename Number >

void MeltPoolDG::CompressibleFlow::calculate_penalty_parameter	(	dealii::AlignedVector< dealii::VectorizedArray< Number > > &	array_penalty_parameter,
		const dealii::MatrixFree< dim, Number > &	matrix_free,
		const std::string &	domain_representation_type,
		const unsigned int	dof_index = 0,
		const Number	scaling_factor = 1.0
	)

This function computes the local values of the internal penalty parameter used in the viscous numerical flux.

Parameters

array_penalty_parameter	Array in which the values of the penalty parameter are stored.
matrix_free	Matrix-free object providing the required geometrical data.
domain_representation_type	Numerical operator type (cut or fitted_mesh).
dof_index	Index of the relevant dof handler in the matrix-free object.
scaling_factor	Additional scaling factor to scale the penalty parameter.

calculate_velocity()

template<int dim, typename number >

DEAL_II_ALWAYS_INLINE dealii::Tensor< 1, dim, dealii::VectorizedArray< number > > MeltPoolDG::CompressibleFlow::calculate_velocity ( const ConservedVariablesType< dim, number > &  conserved_variables )

inline

Calculate the velocity from the conserved variables by computing u = (ρu)/ρ.

Parameters

conserved_variables

Current values of the conserved variables.

Returns

Current velocity.

convective_flux()

template<int dim, typename ConservedVariablesView , typename WritableFluxView >

DEAL_II_ALWAYS_INLINE void MeltPoolDG::CompressibleFlow::convective_flux ( const ConservedVariablesView &  conserved_variables, const WritableFluxView &  flux  )

inline

Calculate the convective flux F_c for the compressible Navier-Stokes equations.

Parameters

conserved_variables

View on the local values of the conserved variables, providing convenient accessor functions for the quantities needed to compute the convective flux.

Template Parameters

value_type

Type of the conserved variables.

diffusive_flux()

template<int dim, typename VectorizedArrayType , typename DofStateView , typename WritableFluxView >

DEAL_II_ALWAYS_INLINE void MeltPoolDG::CompressibleFlow::diffusive_flux ( const DofStateView &  conserved_variables, const WritableFluxView &  flux  )

inline

Calculate the diffusive (viscous) flux F_d for the compressible Navier-Stokes equations.

Parameters

conserved_variables

A view on the local values of the conserved variables and their gradients, providing convenient accessor functions for the quantities needed to compute the diffusive flux, such as velocity, velocity gradients, temperature gradients, dynamic viscosity, and thermal conductivity.

Template Parameters

value_type	Type of the conserved variables.
gradient_type	Type of the gradients of the conserved variables.

maximum_local_wave_speed()

template<typename DofViewType , typename VectorizedArrayType >

DEAL_II_ALWAYS_INLINE VectorizedArrayType MeltPoolDG::CompressibleFlow::maximum_local_wave_speed ( const DofViewType &  u_m, const DofViewType &  u_p  )

inline

rhs_boundary_face_integral_kernel()

template<int dim, typename number , FaceEvaluatorType< dim, dim+2, number, dealii::VectorizedArray< number > > Integrator, bool is_viscous = true, bool is_gas_phase = true>

DEAL_II_ALWAYS_INLINE std::tuple< ConservedVariablesType< dim, number >, ConservedVariablesGradientType< dim, number > > MeltPoolDG::CompressibleFlow::rhs_boundary_face_integral_kernel ( const Integrator &  evaluator_m, const unsigned int  q, const dealii::types::boundary_id  boundary_id, const dealii::VectorizedArray< number >  penalty_parameter, const ConvectiveKernels< dim, number > &  convective_terms, const ViscousKernels< dim, number > &  viscous_terms, const Material< dim, number > &  material, const BoundaryConditions< dim, number > &  boundary_conditions  )

inline

Computes the right-hand side boundary face integral kernels at a boundary face quadrature point.

Kernel of the local boundary face applier for the right-hand side function. This function computes the face integral contribution of boundary faces to the right hand side for the quadrature point index and the corresponding FE evaluator.

Parameters

evaluator_m	FE-evaluator object reinitialized on the current (inner) face batch.
q	Index of the quadrature point.
boundary_id	Boundary ID of the considered boundary face.
penalty_parameter	Value of the symmetric interior penalty parameter on the face.
convective_terms	Collection of convective term computations for the compressible Navier-Stokes equations.
viscous_terms	Collection of viscous term computations for the compressible Navier-Stokes equations.
material	Class providing material data and calculations of thermodynamic relations.
boundary_conditions	Class providing boundary condition related computations for the compressible flow solver

Returns

Tuple, containing the flux for the boundary face, weighted with the value of the test function, as first argument, and the flux for the boundary face, weighted with the gradient of the test function, as second argument.

rhs_cell_integral_kernel()

template<int dim, typename number , CellEvaluatorType< dim, dim+2, number, dealii::VectorizedArray< number > > Integrator, bool is_viscous = true>

DEAL_II_ALWAYS_INLINE std::tuple< ConservedVariablesType< dim, number >, ConservedVariablesGradientType< dim, number > > MeltPoolDG::CompressibleFlow::rhs_cell_integral_kernel ( const Integrator &  evaluator, const unsigned int  q, const dealii::Tensor< 1, dim, dealii::VectorizedArray< number > > *  constant_body_force, const ConvectiveKernels< dim, number > &  convective_terms, const ViscousKernels< dim, number > &  viscous_terms, const std::unique_ptr< dealii::Function< dim > > &  body_force  )

inline

Computes the right-hand side cell integral kernels at a quadrature point.

Kernel of the local cell applier for the right-hand side function. This function computes the cell integral contribution to the right hand side for the quadrature point index and the corresponding FE evaluator.

Parameters

evaluator	FE-evaluator object reinitialized on the current cell batch.
q	Index of the quadrature point.
constant_body_force	Value of the body force. If the body force is not constant the pointer must be set to nullptr.
convective_terms	Collection of convective term computations for the compressible Navier-Stokes equations.
viscous_terms	Collection of viscous term computations for the compressible Navier-Stokes equations.
body_force	Pointer to a body force function.

Returns

Tuple, containing the flux, weighted with the value of the test function, as first argument, and the flux, weighted with the gradient of the test function, as second argument.

rhs_face_integral_kernel()

template<int dim, typename number , FaceEvaluatorType< dim, dim+2, number, dealii::VectorizedArray< number > > Integrator, bool is_viscous = true>

DEAL_II_ALWAYS_INLINE std::tuple< ConservedVariablesType< dim, number >, ConservedVariablesType< dim, number >, ConservedVariablesGradientType< dim, number >, ConservedVariablesGradientType< dim, number > > MeltPoolDG::CompressibleFlow::rhs_face_integral_kernel ( const Integrator &  evaluator_m, const Integrator &  evaluator_p, const unsigned int  q, dealii::VectorizedArray< number >  penalty_parameter, const ConvectiveKernels< dim, number > &  convective_terms, const ViscousKernels< dim, number > &  viscous_terms  )

inline

Computes the right-hand side face integral kernels at a face quadrature point.

Kernel of the local inner face applier for the right-hand side function. This function computes the face integral contribution of inner faces to the right hand side for the quadrature point index and the corresponding FE evaluator.

Parameters

evaluator_m	FE-evaluator object reinitialized on the current (inside) face batch.
evaluator_p	FE-evaluator object reinitialized on the current (outside) face batch.
q	Index of the quadrature point.
penalty_parameter	Value of the symmetric interior penalty parameter on the face.
convective_terms	Collection of convective term computations for the compressible Navier-Stokes equations.
viscous_terms	Collection of viscous term computations for the compressible Navier-Stokes equations.

Returns

Tuple, which containing the fluxes for the inside and outside faces, weighted with the value of the test functions, as first two arguments, and the fluxes for the inside and outside faces, weighted with the gradient of the test functions, as the third and fourth argument.

update_primitive_variables_solution()

template<int dim, typename number >

void MeltPoolDG::CompressibleFlow::update_primitive_variables_solution	(	dealii::LinearAlgebra::distributed::Vector< number > &	solution_primitive_variables,
		const dealii::LinearAlgebra::distributed::Vector< number > &	solution,
		const ScratchData< dim, dim, number > &	scratch_data,
		const unsigned int	dof_idx,
		const unsigned int	quad_idx,
		const Material< dim, number > *	material_liquid,
		const Material< dim, number > *	material_gas = nullptr
	)

Update the primitive variable solution according to the current solution vector.

Parameters

solution_primitive_variables	Vector where the solution in primitive variables is stored.
solution	Current solution vector in conservative variable formulation.
dof_idx	Index of the relevant dof handler in the matrix-free object.
quad_idx	Relevant quadrature index of the flow solver.
material_liquid	Pointer to the material object for liquid phase.
material_gas	Pointer to the material object for the gas phase.

Note

The second material object is only required for the two-phase case.

viscous_stress_tensor()

template<int dim, typename number >

DEAL_II_ALWAYS_INLINE dealii::Tensor< 1, dim, dealii::Tensor< 1, dim, dealii::VectorizedArray< number > > > MeltPoolDG::CompressibleFlow::viscous_stress_tensor ( const dealii::Tensor< 1, dim, dealii::Tensor< 1, dim, dealii::VectorizedArray< number > > > &  grad_velocity, const dealii::VectorizedArray< number >  dynamic_viscosity  )

inline

Calculate the viscous stress tensor for the compressible Navier-Stokes equations.

Parameters

grad_velocity	Gradient of the velocity field.
dynamic_viscosity	Dynamic viscosity of the fluid.

Variable Documentation

analytic

MeltPoolDG::CompressibleFlow::analytic

char

MeltPoolDG::CompressibleFlow::char

complete_fd

MeltPoolDG::CompressibleFlow::complete_fd

lambda_fd

MeltPoolDG::CompressibleFlow::lambda_fd

n_conserved_variables

template<int dim, int n_species = 1>

constexpr unsigned int MeltPoolDG::CompressibleFlow::n_conserved_variables = dim + 2 + (n_species - 1)

constexpr

Number of independent conserved variables for the compressible Navier-Stokes equations in dim dimensions.