OpenFoam Transition modelling : kklOmega

Ranjan · August 12, 2015, 20:36

Hello Foamers

I am currently working on a case in which I need to get near accurate cl & cd data for a 4 digit NACA airfoil at Re 500,000. I have used simpleFoam earlier and found it to be accurate only in the pre stall regime.

I have setup the case in pimpleFoam and I intend to use kklOmega turbulence model. However, even though there are a few literature resources, I am not able to figure out the correct numeric schemes.

Can anybody advice ?

Thanks in advance

msuaeronautics · August 13, 2015, 21:52

What schemes did you use in your simpleFoam cases? Could you provide some figures?

August 12, 2015, 20:36	OpenFoam Transition modelling : kklOmega	#1
Ranjan New Member Ranjan Join Date: Apr 2014 Posts: 29 Rep Power: 12	Hello Foamers I am currently working on a case in which I need to get near accurate cl & cd data for a 4 digit NACA airfoil at Re 500,000. I have used simpleFoam earlier and found it to be accurate only in the pre stall regime. I have setup the case in pimpleFoam and I intend to use kklOmega turbulence model. However, even though there are a few literature resources, I am not able to figure out the correct numeric schemes. Can anybody advice ? Thanks in advance

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August 13, 2015, 21:52		#2
msuaeronautics Member Eric Robertson Join Date: Jul 2012 Posts: 95 Rep Power: 15	What schemes did you use in your simpleFoam cases? Could you provide some figures?