Fluent setup for Renolds No of 0.15 to 0.7 milion
hello every body : I have confused what model to use for low reynolds numbe r flow around the german low speed airfoil FX . I used K-omega and K epsilon modles but the drag was about 50 % dieffrent from EXPerimental (dated both at 1930 and 2004). results
I want the fluent set up model for low Re. number as 150,000 to 500,000. I mean is laminer flow ok? or Some turbulance modle is better?
thanks M. Essuri
Re: Fluent setup for Renolds No of 0.15 to 0.7 mil
Hi, You can try with the Spalart Allmaras model. It was developed to work with aerospace applications.
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