Hello Everyone ,
Hope you are doing great .
I am simulating a 3D wing of aspect ratios
a) 0.5
b)1
c)1.5
d) 2
Why is it so that as I move from AR=0 to AR=2 the difference between CFD and experimental results increases .
Regards
Aamir Sultan
@ AR = Wing Span / Mean Chord Length Horimek Abderrahmane
Horimek Abderrahmane I have done grid independence for all four meshes .
Horimek Abderrahmane you are right , I have done grid independence for only low angle of attacks . I will refine my mesh for higher angle of attacks and will see how it goes .
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