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Search: Posts Made By: pcasto
Forum: OpenFOAM Running, Solving & CFD July 24, 2008, 23:56
Replies: 20
Views: 4,391
Posted By pcasto
For anyone interested in analy

For anyone interested in analyzing an airfoil with simpleFoam or rhoSimpleFoam, I posted my case folders for a Naca0012 at 2 degrees AOA. Hope this can be useful to people reading this thread. I used...
Forum: OpenFOAM Running, Solving & CFD July 16, 2008, 15:16
Replies: 20
Views: 4,391
Posted By pcasto
Hey Paulo, No I haven't cal

Hey Paulo,

No I haven't calculated Cl and Cd yet. I will probably do that soon. I'll let you know what are my results. I am now trying to simulate the flow at higher angle of attach but I'm...
Forum: OpenFOAM Running, Solving & CFD July 12, 2008, 18:24
Replies: 20
Views: 4,391
Posted By pcasto
Hey Paulo, Thanx for your r

Hey Paulo,

Thanx for your reply. I finally managed to have icoFoam converged. I also tried using simpleFoam and you are right, switching turbulence on (I used k-epsilon) helps in improving the...
Forum: OpenFOAM Running, Solving & CFD July 9, 2008, 17:59
Replies: 20
Views: 4,391
Posted By pcasto
Hey Paulo, I understand th

Hey Paulo,

I understand that at this Reynolds number, the flow should transition to turbulent flow over the airfoil. However, the algorithm should still be able to converge even though it might...
Forum: OpenFOAM Running, Solving & CFD July 7, 2008, 20:50
Replies: 20
Views: 4,391
Posted By pcasto
Hi everyone, I am trying to

Hi everyone,

I am trying to simulate steady flow over a NACA0012 airfoil at Mach number 0.2 and AOA 2 degrees and I'm having problems converging to the solution with icoFoam.

I'm using a...
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