def createFields(runTime, mesh, pimple):
ref.ext_Info() << "Reading thermophysical properties\n" << ref.nl
pThermo = man.basicPsiThermo.New(mesh)
p = man.volScalarField(pThermo.p(), man.Deps(pThermo))
h = man.volScalarField(pThermo.h(), man.Deps(pThermo))
psi = man.volScalarField(pThermo.psi(), man.Deps(pThermo))
rho = man.volScalarField(
man.IOobject(ref.word("rho"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.READ_IF_PRESENT, ref.IOobject.AUTO_WRITE),
man.volScalarField(pThermo.rho(), man.Deps(pThermo)))
ref.ext_Info() << "Reading field U\n" << ref.nl
U = man.volVectorField(
man.IOobject(ref.word("U"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.MUST_READ, ref.IOobject.AUTO_WRITE), mesh)
phi = man.compressibleCreatePhi(runTime, mesh, U, rho)
rhoMax = ref.dimensionedScalar(pimple.dict().lookup(ref.word("rhoMax")))
rhoMin = ref.dimensionedScalar(pimple.dict().lookup(ref.word("rhoMin")))
ref.ext_Info() << "Creating turbulence model\n" << ref.nl
turbulence = man.compressible.turbulenceModel.New(rho, U, phi, pThermo)
ref.ext_Info() << "Creating field dpdt\n" << ref.nl
dpdt = man.volScalarField(ref.word("dpdt"), man.fvc.ddt(p))
ref.ext_Info() << "Creating field kinetic energy K\n" << ref.nl
K = man.volScalarField(ref.word("K"),
man.volScalarField(0.5 * U.magSqr(), man.Deps(U)))
return pThermo, p, h, psi, rho, U, phi, rhoMax, rhoMin, turbulence, dpdt, K
def createFields(runTime, mesh):
ref.ext_Info() << "Reading thermophysical properties\n" << ref.nl
pThermo = man.basicPsiThermo.New(mesh)
p = man.volScalarField(pThermo.p(), man.Deps(pThermo))
e = man.volScalarField(pThermo.e(), man.Deps(pThermo))
psi = man.volScalarField(pThermo.psi(), man.Deps(pThermo))
rho = man.volScalarField(
man.IOobject(ref.word("rho"), ref.fileName(runTime.timeName()), mesh),
man.volScalarField(pThermo.rho(), man.Deps(pThermo)))
ref.ext_Info() << "Reading field U\n" << ref.nl
U = man.volVectorField(
man.IOobject(ref.word("U"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.MUST_READ, ref.IOobject.AUTO_WRITE), mesh)
phi = man.compressibleCreatePhi(runTime, mesh, rho, U)
ref.ext_Info() << "Creating turbulence model\n" << ref.nl
turbulence = man.compressible.turbulenceModel.New(rho, U, phi, pThermo)
return pThermo, p, e, psi, rho, U, phi, turbulence
def fun_Ueqn(simple, mesh, rho, U, phi, turbulence, ghf, p_rgh):
UEqn = man.fvm.div(phi, U) + man(turbulence.divDevRhoReff(U),
man.Deps(turbulence, U))
UEqn.relax()
if simple.momentumPredictor():
ref.solve(UEqn == man.fvc.reconstruct((
(-ghf * man.fvc.snGrad(rho) - man.fvc.snGrad(p_rgh)) *
man.surfaceScalarField(mesh.magSf(), man.Deps(mesh)))))
return UEqn
def fun_Ueqn(pimple, mesh, rho, U, phi, turbulence, ghf, p_rgh):
# Solve the Momentum equation
UEqn = man.fvm.ddt(rho, U) + man.fvm.div(phi, U) + man.fvVectorMatrix(
turbulence.divDevRhoReff(U()), man.Deps(turbulence, U))
UEqn.relax()
if pimple.momentumPredictor():
ref.solve(UEqn == man.fvc.reconstruct(
(-ghf * man.fvc.snGrad(rho) - man.fvc.snGrad(p_rgh)) *
man.surfaceScalarField(mesh.magSf(), man.Deps(mesh))))
return UEqn
def fun_UEqn(U, phi, turbulence, p, sources):
# Solve the Momentum equation
UEqn = man.fvm.div(phi, U) + man(turbulence.divDevReff(U),
man.Deps(turbulence, U)) == man(
sources(U), man.Deps(U))
UEqn.relax()
sources.constrain(UEqn)
ref.solve(UEqn == -man.fvc.grad(p))
return UEqn
def setRegionSolidFields( i, solidRegions, thermos ):
mesh = solidRegions[ i ]
thermo = thermos[ i ]
rho = man.volScalarField( thermo.rho(), man.Deps( thermo ) )
cp = man.volScalarField( thermo.Cp(), man.Deps( thermo ) )
kappa = man.volScalarField( thermo.K(), man.Deps( thermo ) )
# tmp<volSymmTensorField> tK = thermo.directionalK();
# const volSymmTensorField& K = tK();
T = man.volScalarField( thermo.T(), man.Deps( thermo ) )
return mesh, thermo, rho, cp, kappa, T
def Ueqn( mesh, pimple, phi, U, p, turbulence, sources ):
UEqn = man.fvm.ddt(U) + man.fvm.div(phi, U) + man.fvVectorMatrix( turbulence.divDevReff( U ), man.Deps( turbulence, U ) ) \
== man.fvVectorMatrix( sources(U), man.Deps( U ) )
UEqn.relax()
sources.constrain( UEqn )
rAU = man.volScalarField( 1.0/UEqn.A(), man.Deps( UEqn ) )
if pimple.momentumPredictor():
ref.solve( UEqn == -man.fvc.grad( p ) )
pass
return UEqn, rAU
def _createFields(runTime, mesh, potentialFlow, args):
ref.ext_Info() << "Reading field p\n" << ref.nl
p = man.volScalarField(
man.IOobject(ref.word("p"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.MUST_READ, ref.IOobject.NO_WRITE), mesh)
p << ref.dimensionedScalar(ref.word("zero"), p.dimensions(), 0.0)
ref.ext_Info() << "Reading field U\n" << ref.nl
U = man.volVectorField(
man.IOobject(ref.word("U"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.MUST_READ, ref.IOobject.AUTO_WRITE), mesh)
U << ref.dimensionedVector(ref.word("0"), U.dimensions(), ref.vector.zero)
phi = man.surfaceScalarField(
man.IOobject(ref.word("phi"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.NO_READ, ref.IOobject.AUTO_WRITE),
man.fvc.interpolate(U)
& man.surfaceVectorField(mesh.Sf(), man.Deps(mesh)))
if args.optionFound(ref.word("initialiseUBCs")):
U.correctBoundaryConditions()
phi << (ref.fvc.interpolate(U) & mesh.Sf())
pass
pRefCell = 0
pRefValue = 0.0
pRefCell, pRefValue = ref.setRefCell(p, potentialFlow, pRefCell, pRefValue)
return p, U, phi, pRefCell, pRefValue
def Ueqn(mesh, pimple, phi, U, p, turbulence, sources):
# The initial C++ expression does not work properly, because of
# 1. turbulence.divDevRhoReff( U ) - changes values for the U boundaries
# 2. the order of expression arguments computation differs with C++
#UEqn = man.fvm.ddt(U) + man.fvm.div(phi, U) + man.fvVectorMatrix( turbulence.divDevReff( U ), man.Deps( turbulence, U ) )
UEqn = man.fvVectorMatrix(turbulence.divDevReff(U), man.Deps(
turbulence, U)) + (man.fvm.ddt(U) + man.fvm.div(phi, U))
UEqn.relax()
sources.constrain(UEqn)
rAU = man.volScalarField(1.0 / UEqn.A(), man.Deps(UEqn))
if pimple.momentumPredictor():
ref.solve(UEqn == -ref.fvc.grad(p) + sources(U))
pass
return UEqn, rAU
def fun_UEqn( mesh, phi, U, p, turbulence, pZones, nUCorr, pressureImplicitPorosity ):
# Construct the Momentum equation
# The initial C++ expression does not work properly, because of
# 1. turbulence.divDevRhoReff( U ) - changes values for the U boundaries
# 2. the order of expression arguments computation differs with C++
#UEqn = fvm.div( phi, U ) + turbulence.divDevReff( U )
UEqn = man.fvVectorMatrix( turbulence.divDevReff( U ), man.Deps( turbulence, U ) ) + man.fvm.div( phi, U )
UEqn.relax()
# Include the porous media resistance and solve the momentum equation
# either implicit in the tensorial resistance or transport using by
# including the spherical part of the resistance in the momentum diagonal
trAU = None
trTU = None
if pressureImplicitPorosity :
tTU = man.volTensorField( ref.tensor( ref.I ) * UEqn.A(), man.Deps( UEqn ) )
pZones.addResistance( UEqn, tTU )
trTU = man.volTensorField( tTU.inv(), man.Deps( tTU ) )
trTU.rename( ref.word( "rAU" ) )
for UCorr in range ( nUCorr ):
U << ( trTU() & ( UEqn.H() - ref.fvc.grad( p ) ) ) # mixed calculations
pass
U.correctBoundaryConditions()
pass
else:
pZones.addResistance( UEqn )
ref.solve( UEqn == -man.fvc.grad( p ) )
trAU = man.volScalarField( 1.0 / UEqn.A(), man.Deps( UEqn ) )
trAU.rename( ref.word( "rAU" ) )
pass
return UEqn, trTU, trAU
def Ueqn(mesh, pimple, phi, U, p, turbulence):
UEqn = man.fvm.ddt(U) + man.fvm.div(phi, U) + man.fvVectorMatrix(
turbulence.divDevReff(U), man.Deps(turbulence, U))
UEqn.relax()
rAU = man.volScalarField(1.0 / UEqn.A(), man.Deps(UEqn))
if pimple.momentumPredictor():
ref.solve(UEqn == -man.fvc.grad(p))
pass
else:
U << rAU * (UEqn.H() - ref.fvc.grad(p))
U.correctBoundaryConditions()
pass
return UEqn, rAU
def _UEqn( phi, U, p, rho, turbulence ):
# Solve the Momentum equation
UEqn = man.fvVectorMatrix( turbulence.divDevRhoReff( U ), man.Deps( turbulence ) ) + man.fvm.div( phi, U )
UEqn.relax()
ref.solve( UEqn == -ref.fvc.grad( p ) )
return UEqn
def _createFields(runTime, mesh):
# Load boundary condition
from BCs import rho
ref.ext_Info() << "Reading thermophysical properties\n" << ref.nl
thermo = man.basicPsiThermo.New(mesh)
p = man.volScalarField(thermo.p(), man.Deps(thermo))
e = man.volScalarField(thermo.e(), man.Deps(thermo))
T = man.volScalarField(thermo.T(), man.Deps(thermo))
psi = man.volScalarField(thermo.psi(), man.Deps(thermo))
mu = man.volScalarField(thermo.mu(), man.Deps(thermo))
inviscid = True
if mu.internalField().max() > 0.0:
inviscid = False
pass
ref.ext_Info() << "Reading field U\n" << ref.nl
U = man.volVectorField(
man.IOobject(ref.word("U"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.MUST_READ, ref.IOobject.AUTO_WRITE), mesh)
pbf, rhoBoundaryTypes = _rhoBoundaryTypes(p)
rho = man.volScalarField(
man.IOobject(ref.word("rho"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.NO_READ, ref.IOobject.AUTO_WRITE),
man.volScalarField(thermo.rho(), man.Deps(thermo)), rhoBoundaryTypes)
rhoU = man.volVectorField(
man.IOobject(ref.word("rhoU"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.NO_READ, ref.IOobject.NO_WRITE), rho * U)
rhoE = man.volScalarField(
man.IOobject(ref.word("rhoE"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.NO_READ, ref.IOobject.NO_WRITE),
rho * (e + man.volScalarField(0.5 * U.magSqr(), man.Deps(U))))
pos = man.surfaceScalarField(
man.IOobject(ref.word("pos"), ref.fileName(runTime.timeName()), mesh),
mesh, ref.dimensionedScalar(ref.word("pos"), ref.dimless, 1.0))
neg = man.surfaceScalarField(
man.IOobject(ref.word("neg"), ref.fileName(runTime.timeName()), mesh),
mesh, ref.dimensionedScalar(ref.word("neg"), ref.dimless, -1.0))
phi = man.surfaceScalarField(
ref.word("phi"),
man.surfaceVectorField(mesh.Sf(), man.Deps(mesh))
& man.fvc.interpolate(rhoU))
ref.ext_Info() << "Creating turbulence model\n" << ref.nl
turbulence = man.compressible.turbulenceModel.New(rho, U, phi, thermo)
return thermo, p, e, T, psi, mu, U, pbf, rhoBoundaryTypes, rho, rhoU, rhoE, pos, neg, inviscid, phi, turbulence
def _createFields( runTime, mesh, simple ):
ref.ext_Info() << "Reading thermophysical properties\n" << ref.nl
thermo = man.basicPsiThermo.New( mesh )
rho = man.volScalarField( man.IOobject( ref.word( "rho" ),
ref.fileName( runTime.timeName() ),
mesh,
ref.IOobject.READ_IF_PRESENT,
ref.IOobject.AUTO_WRITE ),
man.volScalarField( thermo.rho(), man.Deps( thermo ) ) )
p = man.volScalarField( thermo.p(), man.Deps( thermo ) )
h = man.volScalarField( thermo.h(), man.Deps( thermo ) )
psi = man.volScalarField( thermo.psi(), man.Deps( thermo ) )
ref.ext_Info() << "Reading field U\n" << ref.nl
U = man.volVectorField( man.IOobject( ref.word( "U" ),
ref.fileName( runTime.timeName() ),
mesh,
ref.IOobject.MUST_READ,
ref.IOobject.AUTO_WRITE ),
mesh )
phi = man.compressibleCreatePhi( runTime, mesh, rho, U )
pRefCell = 0
pRefValue = 0.0
pRefCell, pRefValue = ref.setRefCell( p, simple.dict(), pRefCell, pRefValue )
rhoMax = ref.dimensionedScalar( simple.dict().lookup( ref.word( "rhoMax" ) ) )
rhoMin = ref.dimensionedScalar( simple.dict().lookup( ref.word( "rhoMin" ) ) )
ref.ext_Info() << "Creating turbulence model\n" << ref.nl
turbulence = man.compressible.RASModel.New( rho,
U,
phi,
thermo )
initialMass = ref.fvc.domainIntegrate( rho )
return thermo, rho, p, h, psi, U, phi, pRefCell, pRefValue, turbulence, initialMass, rhoMax, rhoMin
def fun_UEqn(U, phi, turbulence, p):
# Solve the Momentum equation
UEqn = man.fvm.div(phi, U) + man(turbulence.divDevReff(U),
man.Deps(turbulence, U))
UEqn.relax()
ref.solve(UEqn == -man.fvc.grad(p))
return UEqn
def createPhia(runTime, mesh, Ua):
ref.ext_Info() << "Reading/calculating face flux field phia\n" << ref.nl
phia = man.surfaceScalarField(
man.IOobject(ref.word("phia"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.READ_IF_PRESENT, ref.IOobject.AUTO_WRITE),
man.surfaceScalarField(
ref.linearInterpolate(Ua) & mesh.Sf(), man.Deps(Ua, mesh)))
return phia
def fun_UEqn( mesh, phi, U, p, turbulence, pZones, nUCorr, pressureImplicitPorosity, sources ):
# Construct the Momentum equation
UEqn = man.fvm.div( phi, U ) + man.fvVectorMatrix( turbulence.divDevReff( U ), man.Deps( turbulence, U ) ) == man( sources( U ), man.Deps( U ) )
UEqn.relax()
sources.constrain( UEqn )
# Include the porous media resistance and solve the momentum equation
# either implicit in the tensorial resistance or transport using by
# including the spherical part of the resistance in the momentum diagonal
trAU = None
trTU = None
if pressureImplicitPorosity :
tTU = man.volTensorField( ref.tensor( ref.I ) * UEqn.A(), man.Deps( UEqn ) )
pZones.addResistance( UEqn, tTU )
trTU = man.volTensorField( tTU.inv(), man.Deps( tTU ) )
trTU.rename( ref.word( "rAU" ) )
for UCorr in range ( nUCorr ):
U << ( trTU() & ( UEqn.H() - ref.fvc.grad( p ) ) ) # mixed calculations
pass
U.correctBoundaryConditions()
pass
else:
pZones.addResistance( UEqn )
ref.solve( UEqn == -man.fvc.grad( p ) )
trAU = man.volScalarField( 1.0 / UEqn.A(), man.Deps( UEqn ) )
trAU.rename( ref.word( "rAU" ) )
pass
return UEqn, trTU, trAU
def _UEqn(mesh, alpha1, U, p, p_rgh, ghf, rho, rhoPhi, turbulence, g,
twoPhaseProperties, interface, pimple):
muEff = man.surfaceScalarField(
ref.word("muEff"),
man.surfaceScalarField(twoPhaseProperties.muf(),
man.Deps(twoPhaseProperties)) +
man.fvc.interpolate(rho * man.volScalarField(turbulence.ext_nut(),
man.Deps(turbulence))))
UEqn = man.fvm.ddt(rho, U) + man.fvm.div(rhoPhi, U) - man.fvm.laplacian(
muEff, U) - (man.fvc.grad(U) & man.fvc.grad(muEff))
UEqn.relax()
if pimple.momentumPredictor():
ref.solve( UEqn == \
ref.fvc.reconstruct( ( ref.fvc.interpolate( interface.sigmaK() ) * ref.fvc.snGrad( alpha1 ) - ghf * ref.fvc.snGrad( rho ) \
- ref.fvc.snGrad( p_rgh ) ) * mesh.magSf() ) )
pass
return UEqn
def fun_UrelEqn(Urel, phi, turbulence, p, sources, SRF):
# Solve the Momentum equation
UrelEqn = man.fvVectorMatrix( ref.fvm.div( phi, Urel ) + turbulence.divDevReff( Urel ) + SRF.Su(), man.Deps( turbulence, Urel, phi, SRF ) ) \
== man( sources( Urel ), man.Deps( Urel ) )
UrelEqn.relax()
sources.constrain(UrelEqn)
ref.solve(UrelEqn == -man.fvc.grad(p))
return UrelEqn
def _createFields( runTime, mesh ):
ref.ext_Info() << "Reading field p\n" << ref.nl
p = man.volScalarField( man.IOobject( ref.word( "p" ),
ref.fileName( runTime.timeName() ),
mesh,
ref.IOobject.MUST_READ,
ref.IOobject.AUTO_WRITE ),
mesh )
ref.ext_Info() << "Reading field Urel\n" << ref.nl
Urel = man.volVectorField( man.IOobject( ref.word( "Urel" ),
ref.fileName( runTime.timeName() ),
mesh,
ref.IOobject.MUST_READ,
ref.IOobject.AUTO_WRITE ),
mesh )
ref.ext_Info() << "Reading/calculating face flux field phi\n" << ref.nl
phi = man.surfaceScalarField( man.IOobject( ref.word( "phi" ),
ref.fileName( runTime.timeName() ),
mesh,
ref.IOobject.READ_IF_PRESENT,
ref.IOobject.AUTO_WRITE ),
man.surfaceScalarField( ref.linearInterpolate( Urel ) & mesh.Sf(), man.Deps( mesh, Urel ) ) )
pRefCell = 0
pRefValue = 0.0
pRefCell, pRefValue = ref.setRefCell( p, mesh.solutionDict().subDict( ref.word( "PIMPLE" ) ), pRefCell, pRefValue )
laminarTransport = man.singlePhaseTransportModel( Urel, phi )
turbulence = man.incompressible.turbulenceModel.New( Urel, phi, laminarTransport )
ref.ext_Info() << "Creating SRF model\n" << ref.nl
SRF = man.SRF.SRFModel.New( Urel )
sources = man.IObasicSourceList( mesh )
# Create the absolute velocity
U = man.volVectorField( man.IOobject( ref.word( "U" ),
ref.fileName( runTime.timeName() ),
mesh,
ref.IOobject.NO_READ,
ref.IOobject.AUTO_WRITE ),
man.volVectorField( Urel() + SRF.U(), man.Deps( Urel, SRF ) ) ) # mixed calculations
return p, U, Urel, SRF, phi, turbulence, pRefCell, pRefValue, laminarTransport, sources
def createFields( runTime, mesh ):
ref.ext_Info()<< "Reading thermophysical properties\n" << ref.nl
pThermo = man.basicPsiThermo.New( mesh )
p = man.volScalarField( pThermo.p(), man.Deps( pThermo ) )
h = man.volScalarField( pThermo.h(), man.Deps( pThermo ) )
psi = man.volScalarField( pThermo.psi(), man.Deps( pThermo ) )
rho = man.volScalarField( man.IOobject( ref.word( "rho" ),
ref.fileName( runTime.timeName() ),
mesh,
ref.IOobject.READ_IF_PRESENT,
ref.IOobject.AUTO_WRITE ),
man.volScalarField( pThermo.rho(), man.Deps( pThermo ) ) )
ref.ext_Info()<< "Reading field U\n" << ref.nl
U = man.volVectorField( man.IOobject( ref.word( "U" ),
ref.fileName( runTime.timeName() ),
mesh,
ref.IOobject.MUST_READ,
ref.IOobject.AUTO_WRITE ),
mesh )
phi = man.compressibleCreatePhi( runTime, mesh, U, rho )
rhoMax = ref.dimensionedScalar( mesh.solutionDict().subDict( ref.word( "PIMPLE" ) ).lookup( ref.word( "rhoMax" ) ) )
rhoMin = ref.dimensionedScalar( mesh.solutionDict().subDict( ref.word( "PIMPLE" ) ).lookup( ref.word( "rhoMin" ) ) )
ref.ext_Info()<< "Creating turbulence model\n" << ref.nl
turbulence = man.compressible.turbulenceModel.New( rho, U, phi, pThermo );
ref.ext_Info()<< "Creating field DpDt\n" << ref.nl;
DpDt = man.fvc.DDt( man.surfaceScalarField( ref.word( "phiU" ), phi / man.fvc.interpolate( rho ) ), p )
return pThermo, p, h, psi, rho, U, phi, rhoMax, rhoMin, turbulence, DpDt
def fun_UEqn(rho, U, phi, ghf, p_rgh, turb, mesh, momentumPredictor,
finalIter):
# Solve the Momentum equation
UEqn = man.fvm.ddt(rho, U) + man.fvm.div(phi, U) + man.fvVectorMatrix(
turb.divDevRhoReff(U), man.Deps(turb, U))
UEqn.relax()
if momentumPredictor:
ref.solve(
UEqn() == ref.fvc.reconstruct(
(-ghf * ref.fvc.snGrad(rho) - ref.fvc.snGrad(p_rgh)) *
mesh.magSf()), mesh.solver(U.select(finalIter)))
pass
return UEqn
def fun_UEqn(mesh, phi, U, p, rAU, turbulence, pimple):
# The initial C++ expression does not work properly, because of
# 1. turbulence.divDevRhoReff( U ) - changes values for the U boundaries
# 2. the order of expression arguments computation differs with C++
# UEqn = man.fvm.ddt(U) + man.fvm.div(phi, U) + man.fvVectorMatrix( turbulence.divDevReff( U ), man.Deps( turbulence, U ) )
UEqn = man.fvVectorMatrix(turbulence.divDevReff(U), man.Deps(
turbulence, U)) + (man.fvm.ddt(U) + man.fvm.div(phi, U))
UEqn.relax()
rAU << 1.0 / UEqn.A()
if pimple.momentumPredictor():
ref.solve(UEqn() == -ref.fvc.grad(p))
pass
return UEqn
def _UrelEqn( mesh, pimple, phi, Urel, p, turbulence, SRF, sources ):
# Relative momentum predictor
# The initial C++ expression does not work properly, because of
# 1. turbulence.divDevRhoReff( U ) - changes values for the U boundaries
# 2. the order of expression arguments computation differs with C++
# UrelEqn = man.fvVectorMatrix( ref.fvm.ddt( Urel ) + ref.fvm.div( phi, Urel ) + turbulence.divDevReff( Urel ) + SRF.Su(), \
# man.Deps( phi, Urel, turbulence, SRF ) );
UrelEqn = man.fvVectorMatrix( turbulence.divDevReff( Urel ) + ref.fvm.div( phi, Urel ) + ref.fvm.ddt( Urel ) + SRF.Su(), \
man.Deps( phi, Urel, turbulence, SRF ) );
UrelEqn.relax()
sources.constrain( UrelEqn )
ref.solve( UrelEqn == -ref.fvc.grad( p ) + sources( Urel ) )
return UrelEqn
def createFields(runTime, mesh, g):
ref.ext_Info() << "Reading thermophysical properties\n" << ref.nl
pThermo = man.basicRhoThermo.New(mesh)
rho = man.volScalarField(
man.IOobject(ref.word("rho"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.NO_READ, ref.IOobject.NO_WRITE),
man.volScalarField(pThermo.rho(), man.Deps(pThermo)))
p = man.volScalarField(pThermo.p(), man.Deps(pThermo))
h = man.volScalarField(pThermo.h(), man.Deps(pThermo))
psi = man.volScalarField(pThermo.psi(), man.Deps(pThermo))
ref.ext_Info() << "Reading field U\n" << ref.nl
U = man.volVectorField(
man.IOobject(ref.word("U"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.MUST_READ, ref.IOobject.AUTO_WRITE), mesh)
phi = man.compressibleCreatePhi(runTime, mesh, U, rho)
ref.ext_Info() << "Creating turbulence model\n" << ref.nl
turbulence = man.compressible.turbulenceModel.New(rho, U, phi, pThermo)
ref.ext_Info() << "Calculating field g.h\n" << ref.nl
gh = man.volScalarField(ref.word("gh"),
man.volScalarField(g & mesh.C(), man.Deps(mesh)))
ghf = man.surfaceScalarField(
ref.word("ghf"), man.surfaceScalarField(g & mesh.Cf(), man.Deps(mesh)))
ref.ext_Info() << "Reading field p_rgh\n" << ref.nl
p_rgh = man.volScalarField(
man.IOobject(ref.word("p_rgh"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.MUST_READ, ref.IOobject.AUTO_WRITE), mesh)
# Force p_rgh to be consistent with p
p_rgh << p - rho * gh
ref.ext_Info() << "Creating field dpdt\n" << ref.nl
dpdt = man.volScalarField(ref.word("dpdt"), man.fvc.ddt(p))
ref.ext_Info() << "Creating field kinetic energy K\n" << ref.nl
K = man.volScalarField(ref.word("K"),
man.volScalarField(0.5 * U.magSqr(), man.Deps(U)))
return pThermo, p, rho, h, psi, U, phi, turbulence, gh, ghf, p_rgh, dpdt, K
def createFields(runTime, mesh, g):
ref.ext_Info() << "Reading thermophysical properties\n" << ref.nl
pThermo = man.basicPsiThermo.New(mesh)
rho = man.volScalarField(
man.IOobject(ref.word("rho"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.NO_READ, ref.IOobject.NO_WRITE),
man(pThermo.rho(), man.Deps(pThermo)))
p = man(pThermo.p(), man.Deps(pThermo))
h = man(pThermo.h(), man.Deps(pThermo))
psi = man(pThermo.psi(), man.Deps(pThermo))
ref.ext_Info() << "Reading field U\n" << ref.nl
U = man.volVectorField(
man.IOobject(ref.word("U"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.MUST_READ, ref.IOobject.AUTO_WRITE), mesh)
phi = man.compressibleCreatePhi(runTime, mesh, rho, U)
ref.ext_Info() << "Creating turbulence model\n" << ref.nl
turbulence = man.compressible.RASModel.New(rho, U, phi, pThermo)
ref.ext_Info() << "Calculating field g.h\n" << ref.nl
gh = man.volScalarField(ref.word("gh"), man(g & mesh.C(), man.Deps(mesh)))
ghf = man.surfaceScalarField(ref.word("ghf"),
man(g & mesh.Cf(), man.Deps(mesh)))
ref.ext_Info() << "Reading field p_rgh\n" << ref.nl
p_rgh = man.volScalarField(
man.IOobject(ref.word("p_rgh"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.MUST_READ, ref.IOobject.AUTO_WRITE), mesh)
# Force p_rgh to be consistent with p
p_rgh << p - rho * gh
pRefCell = 0
pRefValue = 0.0
pRefCell, pRefValue = ref.setRefCell(
p, p_rgh,
mesh.solutionDict().subDict(ref.word("SIMPLE")), pRefCell, pRefValue)
initialMass = ref.fvc.domainIntegrate(rho)
totalVolume = mesh.V().ext_sum()
return pThermo, rho, p, h, psi, U, phi, turbulence, gh, ghf, p_rgh, pRefCell, pRefValue, initialMass, totalVolume
def fun_Ueqn( pimple, rho, p, U, phi, turbulence ):
# The initial C++ expression does not work properly, because of
# 1. turbulence.divDevRhoReff( U ) - changes values for the U boundaries
# 2. the order of expression arguments computation differs with C++
# UEqn = man.fvm.ddt( rho, U ) + man.fvm.div( phi, U ) + man.fvVectorMatrix( turbulence.divDevRhoReff( U ), man.Deps( turbulence, U ) )
UEqn = man.fvVectorMatrix( turbulence.divDevRhoReff( U ), man.Deps( turbulence, U ) ) + ( man.fvm.div( phi, U ) + man.fvm.ddt( rho, U ) )
UEqn.relax()
rAU = 1.0 / UEqn.A()
if pimple.momentumPredictor():
ref.solve( UEqn == -man.fvc.grad( p ) )
pass
else:
U << rAU * ( UEqn.H() - ref.fvc.grad( p ) )
U.correctBoundaryConditions()
pass
return UEqn, rAU
def fun_Ueqn(pimple, rho, p, U, phi, turbulence, mrfZones, pZones):
# The initial C++ expression does not work properly, because of
# 1. turbulence.divDevRhoReff( U ) - changes values for the U boundaries
# 2. the order of expression arguments computation differs with C++
# UEqn = man.fvm.ddt( rho, U ) + man.fvm.div( phi, U ) + man.fvVectorMatrix( turbulence.divDevRhoReff( U ), man.Deps( turbulence, U ) )
UEqn = man.fvVectorMatrix(
turbulence.divDevRhoReff(U), man.Deps(
turbulence, U)) + (man.fvm.div(phi, U) + man.fvm.ddt(rho, U))
UEqn.relax()
mrfZones.addCoriolis(rho, UEqn)
pZones.addResistance(UEqn)
rAU = 1.0 / UEqn.A()
if pimple.momentumPredictor():
ref.solve(UEqn == -man.fvc.grad(p))
pass
return UEqn
def compressibleCreatePhiHolder(runTime, mesh, rho, U):
from Foam import man
return man(compressibleCreatePhi(runTime, mesh, rho, U),
man.Deps(runTime, mesh, rho, U))
def _createFields(runTime, mesh):
ref.ext_Info() << "Reading field p_rgh\n" << ref.nl
p_rgh = man.volScalarField(
man.IOobject(ref.word("p_rgh"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.MUST_READ, ref.IOobject.AUTO_WRITE), mesh)
ref.ext_Info() << "Reading field alpha1\n" << ref.nl
man.interfaceProperties # Load corresponding library to be able to use the following BC - "constantAlphaContactAngleFvPatchScalarField"
alpha1 = man.volScalarField(
man.IOobject(ref.word("alpha1"), ref.fileName(runTime.timeName()),
mesh, ref.IOobject.MUST_READ, ref.IOobject.AUTO_WRITE),
mesh)
ref.ext_Info() << "Reading field U\n" << ref.nl
U = man.volVectorField(
man.IOobject(ref.word("U"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.MUST_READ, ref.IOobject.AUTO_WRITE), mesh)
phi = man.createPhi(runTime, mesh, U)
ref.ext_Info() << "Reading transportProperties\n" << ref.nl
twoPhaseProperties = man.twoPhaseMixture(U, phi)
rho1 = twoPhaseProperties.rho1()
rho2 = twoPhaseProperties.rho2()
# Need to store rho for ddt(rho, U)
rho = man.volScalarField(
man.IOobject(ref.word("rho"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.READ_IF_PRESENT),
alpha1 * rho1 + (1.0 - alpha1) * rho2,
alpha1.ext_boundaryField().types())
rho.oldTime()
# Mass flux
# Initialisation does not matter because rhoPhi is reset after the
# alpha1 solution before it is used in the U equation.
rhoPhi = man.surfaceScalarField(
man.IOobject(ref.word("rho*phi"), ref.fileName(runTime.timeName()),
mesh, ref.IOobject.NO_READ, ref.IOobject.NO_WRITE),
rho1 * phi)
# Construct interface from alpha1 distribution
interface = man.interfaceProperties(alpha1, U, twoPhaseProperties)
# Construct incompressible turbulence model
turbulence = man.incompressible.turbulenceModel.New(
U, phi, twoPhaseProperties)
g = man.readGravitationalAcceleration(runTime, mesh)
#dimensionedVector g0(g);
#Read the data file and initialise the interpolation table
#interpolationTable<vector> timeSeriesAcceleration( runTime.path()/runTime.caseConstant()/"acceleration.dat" );
ref.ext_Info() << "Calculating field g.h\n" << ref.nl
gh = man.volScalarField(ref.word("gh"),
g & man.volVectorField(mesh.C(), man.Deps(mesh)))
ghf = man.surfaceScalarField(
ref.word("ghf"), g & man.surfaceVectorField(mesh.Cf(), man.Deps(mesh)))
p = man.volScalarField(
man.IOobject(ref.word("p"), ref.fileName(runTime.timeName()), mesh,
ref.IOobject.NO_READ, ref.IOobject.AUTO_WRITE),
p_rgh + rho * gh)
pRefCell = 0
pRefValue = 0.0
pRefCell, pRefValue = ref.setRefCell(
p, p_rgh,
mesh.solutionDict().subDict(ref.word("PIMPLE")), pRefCell, pRefValue)
if p_rgh.needReference():
p += ref.dimensionedScalar(
ref.word("p"), p.dimensions(),
pRefValue - ref.getRefCellValue(p, pRefCell))
p_rgh << p - rho * gh
pass
return p_rgh, p, alpha1, U, phi, rho1, rho2, rho, rhoPhi, twoPhaseProperties, pRefCell, pRefValue, interface, turbulence, g, gh, ghf
