Supersonic free stream condition. More...
#include <finiteVolume/supersonicFreestreamFvPatchVectorField.H>
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 zero-gradiented from inside the domain.
N.B. This boundary condition is ill-posed if the free-stream flow is normal to the boundary.
Definition at line 60 of file supersonicFreestreamFvPatchVectorField.H.
Public Member Functions | |
| TypeName ("supersonicFreestream") | |
| Runtime type information. | |
| supersonicFreestreamFvPatchVectorField (const fvPatch &, const DimensionedField< vector, volMesh > &) | |
| Construct from patch and internal field. | |
| supersonicFreestreamFvPatchVectorField (const fvPatch &, const DimensionedField< vector, volMesh > &, const dictionary &) | |
| Construct from patch, internal field and dictionary. | |
| supersonicFreestreamFvPatchVectorField (const supersonicFreestreamFvPatchVectorField &, const fvPatch &, const DimensionedField< vector, volMesh > &, const fvPatchFieldMapper &) | |
| Construct by mapping given supersonicFreestreamFvPatchVectorField. | |
| supersonicFreestreamFvPatchVectorField (const supersonicFreestreamFvPatchVectorField &) | |
| Construct as copy. | |
| virtual tmp< fvPatchVectorField > | clone () const |
| Construct and return a clone. | |
| supersonicFreestreamFvPatchVectorField (const supersonicFreestreamFvPatchVectorField &, const DimensionedField< vector, volMesh > &) | |
| Construct as copy setting internal field reference. | |
| virtual tmp< fvPatchVectorField > | clone (const DimensionedField< vector, volMesh > &iF) const |
| Construct and return a clone setting internal field reference. | |
| const vector & | UInf () const |
| Return the velocity at infinity. | |
| vector & | UInf () |
| Return reference to the velocity at infinity to allow adjustment. | |
| scalar | pInf () const |
| Return the pressure at infinity. | |
| scalar & | pInf () |
| Return reference to the pressure at infinity to allow adjustment. | |
| scalar | TInf () const |
| Return the temperature at infinity. | |
| scalar & | TInf () |
| Return reference to the temperature at infinity. | |
| virtual void | updateCoeffs () |
| Update the coefficients associated with the patch field. | |
| virtual void | write (Ostream &) const |
| Write. | |
| supersonicFreestreamFvPatchVectorField | ( | const fvPatch & | p, |
| const DimensionedField< vector, volMesh > & | iF | ||
| ) |
Construct from patch and internal field.
Definition at line 39 of file supersonicFreestreamFvPatchVectorField.C.
References Vector< scalar >::zero.
Referenced by supersonicFreestreamFvPatchVectorField::clone().
| supersonicFreestreamFvPatchVectorField | ( | const fvPatch & | p, |
| const DimensionedField< vector, volMesh > & | iF, | ||
| const dictionary & | dict | ||
| ) |
Construct from patch, internal field and dictionary.
Definition at line 73 of file supersonicFreestreamFvPatchVectorField.C.
References Foam::exit(), Foam::FatalIOError, FatalIOErrorIn, dictionary::found(), fvPatchField< Type >::operator=(), fvPatch::size(), and Vector< scalar >::zero.
| supersonicFreestreamFvPatchVectorField | ( | const supersonicFreestreamFvPatchVectorField & | ptf, |
| const fvPatch & | p, | ||
| const DimensionedField< vector, volMesh > & | iF, | ||
| const fvPatchFieldMapper & | mapper | ||
| ) |
Construct by mapping given supersonicFreestreamFvPatchVectorField.
onto a new patch
Definition at line 57 of file supersonicFreestreamFvPatchVectorField.C.
| supersonicFreestreamFvPatchVectorField | ( | const supersonicFreestreamFvPatchVectorField & | sfspvf | ) |
Construct as copy.
Definition at line 119 of file supersonicFreestreamFvPatchVectorField.C.
| supersonicFreestreamFvPatchVectorField | ( | const supersonicFreestreamFvPatchVectorField & | sfspvf, |
| const DimensionedField< vector, volMesh > & | iF | ||
| ) |
Construct as copy setting internal field reference.
Definition at line 132 of file supersonicFreestreamFvPatchVectorField.C.
| TypeName | ( | "supersonicFreestream" | ) |
Runtime type information.
|
inlinevirtual |
Construct and return a clone.
Definition at line 119 of file supersonicFreestreamFvPatchVectorField.H.
References supersonicFreestreamFvPatchVectorField::supersonicFreestreamFvPatchVectorField().
|
inlinevirtual |
Construct and return a clone setting internal field reference.
Definition at line 136 of file supersonicFreestreamFvPatchVectorField.H.
References supersonicFreestreamFvPatchVectorField::supersonicFreestreamFvPatchVectorField().
|
inline |
Return the velocity at infinity.
Definition at line 152 of file supersonicFreestreamFvPatchVectorField.H.
|
inline |
Return reference to the velocity at infinity to allow adjustment.
Definition at line 158 of file supersonicFreestreamFvPatchVectorField.H.
|
inline |
Return the pressure at infinity.
Definition at line 164 of file supersonicFreestreamFvPatchVectorField.H.
|
inline |
Return reference to the pressure at infinity to allow adjustment.
Definition at line 170 of file supersonicFreestreamFvPatchVectorField.H.
|
inline |
Return the temperature at infinity.
Definition at line 176 of file supersonicFreestreamFvPatchVectorField.H.
|
inline |
Return reference to the temperature at infinity.
to allow adjustment
Definition at line 183 of file supersonicFreestreamFvPatchVectorField.H.
|
virtual |
Update the coefficients associated with the patch field.
Definition at line 147 of file supersonicFreestreamFvPatchVectorField.C.
References Foam::atan(), Foam::exit(), Foam::FatalError, FatalErrorIn, forAll, Foam::log(), Foam::mag(), Foam::pow(), R, Foam::sqr(), Foam::sqrt(), and U.
|
virtual |
Write.
Definition at line 293 of file supersonicFreestreamFvPatchVectorField.C.
References token::END_STATEMENT, Foam::nl, and Ostream::writeKeyword().