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Search: Posts Made By: nomad
Forum: OpenFOAM Running, Solving & CFD September 6, 2009, 05:51
Replies: 180
Views: 58,754
Posted By nomad
magUInf 55.5 - freestream velocity lRef 0.6 -...

magUInf 55.5 - freestream velocity
lRef 0.6 - chord length of airfoil or diameter of cylinder
Aref 1 - surface area, or chord*span
Forum: OpenFOAM Running, Solving & CFD September 3, 2009, 20:42
Replies: 180
Views: 58,754
Posted By nomad
I'm using SimpleFoam, here's my controlDict file:...

I'm using SimpleFoam, here's my controlDict file:

/*--------------------------------*- C++ -*----------------------------------*\
| ========= | ...
Forum: OpenFOAM Running, Solving & CFD September 2, 2009, 14:22
Replies: 180
Views: 58,754
Posted By nomad
Hey, I'm running OpenFOAM 1.6. The flow looks...

Hey,
I'm running OpenFOAM 1.6. The flow looks reasonable around a symmetric airfoil, but Cl and Cd values are just wrong. Also, solutions don't converge for angled airfoils (5 degrees). I'm running...
Forum: OpenFOAM Running, Solving & CFD September 1, 2009, 16:51
Replies: 180
Views: 58,754
Posted By nomad
incorrect forces on symmetric airfoil

Hi,
I'm trying to calculate forces on a symmetric airfoil. I've set lref to the chord length and Aref to the reference area based on the span (these have been converted from imperial to metric...
Forum: OpenFOAM Running, Solving & CFD August 28, 2009, 14:28
Replies: 180
Views: 58,754
Posted By nomad
It works after adding the following lines : ...

It works after adding the following lines :

outputControl timeStep;
outputInterval 1;
Forum: OpenFOAM Running, Solving & CFD August 28, 2009, 13:02
Replies: 180
Views: 58,754
Posted By nomad
OF1.6 forces error

Hi, I'm using OpenFOAM 1.6 and trying to calculate the forces on an airfoil. I have the following lines at the end of my controlDict file:

functions
(
forces
{
type forces;
functionObjectLibs...
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