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Search: Posts Made By: NRA
Forum: OpenFOAM Running, Solving & CFD February 18, 2017, 09:38
Replies: 9
Views: 1,946
Posted By NRA
Hi Peter, Thanks for pointing that out,...

Hi Peter,

Thanks for pointing that out, perhaps it's about time for me to update to 4.0.

I am currently busy with some other projects but I would like to give the transitional SST model a go...
Forum: OpenFOAM Running, Solving & CFD February 18, 2017, 08:15
Replies: 9
Views: 1,946
Posted By NRA
Hi Peter, Glad you achieved a solution with...

Hi Peter,

Glad you achieved a solution with the kkLOmega.

In my case the kkLOmega was also less accurate in terms of lift coefficient. The predicted value was a bit too high, especially for...
Forum: OpenFOAM Running, Solving & CFD February 16, 2017, 15:29
Replies: 9
Views: 1,946
Posted By NRA
Hi Peter, I wouldn't exactly say I solved...

Hi Peter,

I wouldn't exactly say I solved the problem since I ended up changing my project slightly and instead consider a NACA 0012 airfoil. Thus I was able to (after converting to OF mesh) use...
Forum: OpenFOAM Running, Solving & CFD November 20, 2016, 20:21
Replies: 9
Views: 1,946
Posted By NRA
And here are the rest of the case files

And here are the rest of the case files
Forum: OpenFOAM Running, Solving & CFD November 20, 2016, 20:19
Replies: 9
Views: 1,946
Posted By NRA
kklOmega SimpleFoam divergence, kt kl omega

Hi everyone

I'm fairly new in OpenFoam and I'm trying to do a steady simulation of a NACA0006 airfoil at Re=3*10⁶ and AoA=3 deg. I have chosen the kklOmega turbulence model to try to get a decent...
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