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


Public Member Functions | |
| TypeName ("supersonicFreestream") | |
| Runtime type information. More... | |
| supersonicFreestreamFvPatchVectorField (const fvPatch &, const DimensionedField< vector, volMesh > &, const dictionary &) | |
| Construct from patch, internal field and dictionary. More... | |
| supersonicFreestreamFvPatchVectorField (const supersonicFreestreamFvPatchVectorField &, const fvPatch &, const DimensionedField< vector, volMesh > &, const fieldMapper &) | |
| Construct by mapping given supersonicFreestreamFvPatchVectorField. More... | |
| supersonicFreestreamFvPatchVectorField (const supersonicFreestreamFvPatchVectorField &)=delete | |
| Disallow copy without setting internal field reference. More... | |
| supersonicFreestreamFvPatchVectorField (const supersonicFreestreamFvPatchVectorField &, const DimensionedField< vector, volMesh > &) | |
| Copy constructor setting internal field reference. More... | |
| virtual tmp< fvPatchVectorField > | clone (const DimensionedField< vector, volMesh > &iF) const |
| Construct and return a clone setting internal field reference. More... | |
| const vector & | UInf () const |
| Return the velocity at infinity. More... | |
| vector & | UInf () |
| 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... | |
This boundary condition provides a supersonic free-stream condition.
| Property | Description | Required | Default value |
|---|---|---|---|
T | Temperature field name | no | T |
p | Pressure field name | no | p |
psi | Compressibility field name | no | 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.
Definition at line 123 of file supersonicFreestreamFvPatchVectorField.H.
| supersonicFreestreamFvPatchVectorField | ( | const fvPatch & | p, |
| const DimensionedField< vector, volMesh > & | iF, | ||
| const dictionary & | dict | ||
| ) |
Construct from patch, internal field and dictionary.
Definition at line 33 of file supersonicFreestreamFvPatchVectorField.C.
References dict, DimensionedField< Type, GeoMesh, PrimitiveField >::dimensions(), Foam::exit(), Foam::FatalIOError, FatalIOErrorInFunction, fvPatchField< Type >::operator=(), p, and Foam::Zero.
Referenced by supersonicFreestreamFvPatchVectorField::clone().


| supersonicFreestreamFvPatchVectorField | ( | const supersonicFreestreamFvPatchVectorField & | ptf, |
| const fvPatch & | p, | ||
| const DimensionedField< vector, volMesh > & | iF, | ||
| const fieldMapper & | mapper | ||
| ) |
Construct by mapping given supersonicFreestreamFvPatchVectorField.
onto a new patch
Definition at line 80 of file supersonicFreestreamFvPatchVectorField.C.
|
delete |
Disallow copy without setting internal field reference.
| supersonicFreestreamFvPatchVectorField | ( | const supersonicFreestreamFvPatchVectorField & | sfspvf, |
| const DimensionedField< vector, volMesh > & | iF | ||
| ) |
Copy constructor setting internal field reference.
Definition at line 100 of file supersonicFreestreamFvPatchVectorField.C.
| TypeName | ( | "supersonicFreestream" | ) |
Runtime type information.
|
inlinevirtual |
Construct and return a clone setting internal field reference.
Definition at line 191 of file supersonicFreestreamFvPatchVectorField.H.
References supersonicFreestreamFvPatchVectorField::supersonicFreestreamFvPatchVectorField().

|
inline |
Return the velocity at infinity.
Definition at line 208 of file supersonicFreestreamFvPatchVectorField.H.
|
inline |
Return reference to the velocity at infinity to allow adjustment.
Definition at line 214 of file supersonicFreestreamFvPatchVectorField.H.
|
inline |
Return the pressure at infinity.
Definition at line 220 of file supersonicFreestreamFvPatchVectorField.H.
|
inline |
Return reference to the pressure at infinity to allow adjustment.
Definition at line 226 of file supersonicFreestreamFvPatchVectorField.H.
|
inline |
Return the temperature at infinity.
Definition at line 232 of file supersonicFreestreamFvPatchVectorField.H.
|
inline |
Return reference to the temperature at infinity.
to allow adjustment
Definition at line 239 of file supersonicFreestreamFvPatchVectorField.H.
|
virtual |
Update the coefficients associated with the patch field.
Definition at line 120 of file supersonicFreestreamFvPatchVectorField.C.
References Foam::atan(), Foam::exit(), Foam::FatalError, FatalErrorInFunction, forAll, Foam::log(), Foam::mag(), Foam::pow(), Foam::R(), Foam::sqr(), Foam::sqrt(), and U.

|
virtual |
Write.
Definition at line 256 of file supersonicFreestreamFvPatchVectorField.C.
References fvPatchField< Type >::write(), and Foam::writeEntry().
