1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62
|
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: v1812 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
location "0";
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (2 0 0);
/*
A=[2 1]
M=[28.8504 16.0428]
AFR=17.1256917852
T=300
p=1e5
R=8314.3
rho=p/R/T.*M
U=[2 NaN]
U(2)=rho(1)*U(1)*A(1)/(rho(2)*A(2))/AFR
*/
boundaryField
{
"(walls|cylinder)"
{
type fixedValue;
value uniform (0 0 0);
}
inletAir
{
type fixedValue;
value uniform (2 0 0);
}
inletFuel
{
type fixedValue;
value uniform (0.42003 0 0);
}
outlet
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //
|