supersonicFreestreamFvPatchVectorField Class Reference

This boundary condition provides a supersonic free-stream condition. More...

Inheritance diagram for supersonicFreestreamFvPatchVectorField:
Collaboration diagram for supersonicFreestreamFvPatchVectorField:

Public Member Functions

 TypeName ("supersonicFreestream")
 Runtime type information. More...
 
 supersonicFreestreamFvPatchVectorField (const fvPatch &, const DimensionedField< vector, volMesh > &)
 Construct from patch and internal field. More...
 
 supersonicFreestreamFvPatchVectorField (const fvPatch &, const DimensionedField< vector, volMesh > &, const dictionary &)
 Construct from patch, internal field and dictionary. More...
 
 supersonicFreestreamFvPatchVectorField (const this_bctype &, const fvPatch &, const DimensionedField< vector, volMesh > &, const fvPatchFieldMapper &)
 Construct by mapping onto a new patch. More...
 
 supersonicFreestreamFvPatchVectorField (const this_bctype &, const DimensionedField< vector, volMesh > &)
 Construct as copy setting internal field reference. More...
 
 supersonicFreestreamFvPatchVectorField (const this_bctype &)=delete
 No copy without an internal field. More...
 
virtual tmp< fvPatchField< vector > > clone (const DimensionedField< vector, volMesh > &iF) const
 Clone with an internal field reference. More...
 
const vectorUInf () const
 Return the velocity at infinity. More...
 
vectorUInf ()
 Return reference to the velocity at infinity to allow adjustment. More...
 
scalar pInf () const
 Return the pressure at infinity. More...
 
scalar & pInf ()
 Return reference to the pressure at infinity to allow adjustment. More...
 
scalar TInf () const
 Return the temperature at infinity. More...
 
scalar & TInf ()
 Return reference to the temperature at infinity. More...
 
virtual void updateCoeffs ()
 Update the coefficients associated with the patch field. More...
 
virtual void write (Ostream &) const
 Write. More...
 

Detailed Description

This boundary condition provides a supersonic free-stream condition.

  • supersonic outflow is vented according to ???
  • supersonic inflow is assumed to occur according to the Prandtl-Meyer expansion process.
  • subsonic outflow is applied via a zero-gradient condition from inside the domain.
Usage
Property Description Required Default value
T Temperature field name no T
p Pressure field name no p
psi Compressibility field name no thermo:psi
UInf free-stream velocity yes
pInf free-stream pressure yes
TInf free-stream temperature yes
gamma heat capacity ratio (cp/Cv) yes

Example of the boundary condition specification:

    <patchName>
    {
        type            supersonicFreestream;
        UInf            500;
        pInf            1e4;
        TInf            265;
        gamma           1.4;
    }
Note
This boundary condition is ill-posed if the free-stream flow is normal to the boundary.
Source files

Definition at line 124 of file supersonicFreestreamFvPatchVectorField.H.

Constructor & Destructor Documentation

◆ supersonicFreestreamFvPatchVectorField() [1/5]

Construct from patch and internal field.

◆ supersonicFreestreamFvPatchVectorField() [2/5]

Construct from patch, internal field and dictionary.

◆ supersonicFreestreamFvPatchVectorField() [3/5]

Construct by mapping onto a new patch.

◆ supersonicFreestreamFvPatchVectorField() [4/5]

Construct as copy setting internal field reference.

◆ supersonicFreestreamFvPatchVectorField() [5/5]

No copy without an internal field.

Member Function Documentation

◆ TypeName()

TypeName ( "supersonicFreestream"  )

Runtime type information.

◆ clone()

virtual tmp<fvPatchField<vector> > clone ( const DimensionedField< vector, volMesh > &  iF) const
inlinevirtual

Clone with an internal field reference.

Definition at line 227 of file supersonicFreestreamFvPatchVectorField.H.

References fvPatchField< Type >::Clone().

Here is the call graph for this function:

◆ UInf() [1/2]

const vector& UInf ( ) const
inline

Return the velocity at infinity.

Definition at line 242 of file supersonicFreestreamFvPatchVectorField.H.

◆ UInf() [2/2]

vector& UInf ( )
inline

Return reference to the velocity at infinity to allow adjustment.

Definition at line 250 of file supersonicFreestreamFvPatchVectorField.H.

◆ pInf() [1/2]

scalar pInf ( ) const
inline

Return the pressure at infinity.

Definition at line 258 of file supersonicFreestreamFvPatchVectorField.H.

◆ pInf() [2/2]

scalar& pInf ( )
inline

Return reference to the pressure at infinity to allow adjustment.

Definition at line 266 of file supersonicFreestreamFvPatchVectorField.H.

◆ TInf() [1/2]

scalar TInf ( ) const
inline

Return the temperature at infinity.

Definition at line 274 of file supersonicFreestreamFvPatchVectorField.H.

◆ TInf() [2/2]

scalar& TInf ( )
inline

Return reference to the temperature at infinity.

to allow adjustment

Definition at line 284 of file supersonicFreestreamFvPatchVectorField.H.

◆ updateCoeffs()

virtual void updateCoeffs ( )
virtual

Update the coefficients associated with the patch field.

◆ write()

virtual void write ( Ostream ) const
virtual

Write.


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