fvOptions: The "<type>Coeffs" sub-dictionary is now optional

For example the actuationDiskSource fvOption may now be specified

disk1
{
    type            actuationDiskSource;

    fields      (U);

    selectionMode   cellSet;
    cellSet         actuationDisk1;
    diskDir         (1 0 0);    // Orientation of the disk
    Cp              0.386;
    Ct              0.58;
    diskArea        40;
    upstreamPoint   (581849 4785810 1065);
}

rather than

disk1
{
    type            actuationDiskSource;
    active          on;

    actuationDiskSourceCoeffs
    {
        fields      (U);

        selectionMode   cellSet;
        cellSet         actuationDisk1;
        diskDir         (1 0 0);    // Orientation of the disk
        Cp              0.386;
        Ct              0.58;
        diskArea        40;
        upstreamPoint   (581849 4785810 1065);
    }
}

but this form is supported for backward compatibility.
This commit is contained in:
Henry Weller
2017-04-13 13:30:17 +01:00
parent 24b7901d09
commit e3c67dc111
39 changed files with 383 additions and 529 deletions

View File

@ -18,7 +18,6 @@ FoamFile
porosity1
{
type explicitPorositySource;
active yes;
explicitPorositySourceCoeffs
{
@ -27,21 +26,18 @@ porosity1
type DarcyForchheimer;
DarcyForchheimerCoeffs
{
d (2e8 -1000 -1000);
f (0 0 0);
d (2e8 -1000 -1000);
f (0 0 0);
coordinateSystem
coordinateSystem
{
type cartesian;
origin (0 0 0);
coordinateRotation
{
type cartesian;
origin (0 0 0);
coordinateRotation
{
type axesRotation;
e1 (0.70710678 0.70710678 0);
e2 (0 0 1);
}
type axesRotation;
e1 (0.70710678 0.70710678 0);
e2 (0 0 1);
}
}
}

View File

@ -32,15 +32,12 @@ options
{
type scalarSemiImplicitSource;
scalarSemiImplicitSourceCoeffs
{
$injector1;
$injector1;
volumeMode absolute;
injectionRateSuSp
{
thermo:rho.air (1e-3 0); // kg/s
}
volumeMode absolute;
injectionRateSuSp
{
thermo:rho.air (1e-3 0); // kg/s
}
}
@ -48,15 +45,12 @@ options
{
type vectorSemiImplicitSource;
vectorSemiImplicitSourceCoeffs
{
$injector1;
$injector1;
volumeMode absolute;
injectionRateSuSp
{
U.air ((0 -1e-2 0) 0); // kg*m/s^2
}
volumeMode absolute;
injectionRateSuSp
{
U.air ((0 -1e-2 0) 0); // kg*m/s^2
}
}
@ -64,15 +58,12 @@ options
{
type scalarSemiImplicitSource;
scalarSemiImplicitSourceCoeffs
{
$injector1;
$injector1;
volumeMode absolute;
injectionRateSuSp
{
e.air (500 0); // kg*m^2/s^3
}
volumeMode absolute;
injectionRateSuSp
{
e.air (500 0); // kg*m^2/s^3
}
}
}

View File

@ -32,15 +32,12 @@ options
{
type scalarSemiImplicitSource;
scalarSemiImplicitSourceCoeffs
{
$injector1;
$injector1;
volumeMode absolute;
injectionRateSuSp
{
thermo:rho.steam (1.0e-3 0); // kg/s
}
volumeMode absolute;
injectionRateSuSp
{
thermo:rho.steam (1.0e-3 0); // kg/s
}
}
@ -48,15 +45,12 @@ options
{
type vectorSemiImplicitSource;
vectorSemiImplicitSourceCoeffs
{
$injector1;
$injector1;
volumeMode absolute;
injectionRateSuSp
{
U.steam ((0 1e-1 0) 0); // kg*m/s^2
}
volumeMode absolute;
injectionRateSuSp
{
U.steam ((0 1e-1 0) 0); // kg*m/s^2
}
}
@ -64,15 +58,12 @@ options
{
type scalarSemiImplicitSource;
scalarSemiImplicitSourceCoeffs
{
$injector1;
$injector1;
volumeMode absolute;
injectionRateSuSp
{
h.steam (3700 0); // kg*m^2/s^3
}
volumeMode absolute;
injectionRateSuSp
{
h.steam (3700 0); // kg*m^2/s^3
}
}
}

View File

@ -32,15 +32,12 @@ options
{
type scalarSemiImplicitSource;
scalarSemiImplicitSourceCoeffs
{
$injector1;
$injector1;
volumeMode absolute;
injectionRateSuSp
{
thermo:rho.air (1e-3 0); // kg/s
}
volumeMode absolute;
injectionRateSuSp
{
thermo:rho.air (1e-3 0); // kg/s
}
}
@ -48,15 +45,12 @@ options
{
type vectorSemiImplicitSource;
vectorSemiImplicitSourceCoeffs
{
$injector1;
$injector1;
volumeMode absolute;
injectionRateSuSp
{
U.air ((0 -1e-2 0) 0); // kg*m/s^2
}
volumeMode absolute;
injectionRateSuSp
{
U.air ((0 -1e-2 0) 0); // kg*m/s^2
}
}
@ -64,15 +58,12 @@ options
{
type scalarSemiImplicitSource;
scalarSemiImplicitSourceCoeffs
{
$injector1;
$injector1;
volumeMode absolute;
injectionRateSuSp
{
e.air (500 0); // kg*m^2/s^3
}
volumeMode absolute;
injectionRateSuSp
{
e.air (500 0); // kg*m^2/s^3
}
}
}