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July 16, 2010, 11:12 |
How to use rhoSimpleFoam
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#1 |
New Member
Join Date: Jul 2010
Posts: 11
Rep Power: 16 |
Hi OpenFoamers,
I'm a beginner in OpenFoam and I have to compare Fluent and OpenFoam in some studies. Now I want to simulate a flow around an airfoil (NACA 23012) at Mach 0.4. My flow is compressible, the mesh seems to be OK. I have used freestream BC. After 3 iterations, the rho max hardly increases as the bounding k and epsilon. I think I haven't used the solver correctly. I read the user guide and so many topics related to my problem but I didn't find the solution. Can someone help me?? Have a good day to everyone. |
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July 16, 2010, 12:03 |
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#2 |
New Member
Join Date: Jul 2010
Posts: 11
Rep Power: 16 |
For information when I use the model laminar it works well...
So my problem is the configuration of the model k-epsilon... |
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Tags |
airfoil, freestream, naca, rhosimplefoam |
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