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Forum: FLUENT

May 18, 2011, 13:40

Replies: 5

Reasonable error in lift and drag coefficients?

Views: 1,510

Posted By xTamx420

How do you check y+?

How do you check y+?

Forum: FLUENT

May 18, 2011, 08:32

Replies: 5

Reasonable error in lift and drag coefficients?

Views: 1,510

Posted By xTamx420

The solution did converge. I got around 0.009 for...

The solution did converge. I got around 0.009 for Spalart-Allmaras model at a couple different Reynolds Numbers. In Theory of Wing Sections the Cd at 0 angle of attack also is the same number for...

Forum: FLUENT

May 17, 2011, 07:54

Replies: 5

Reasonable error in lift and drag coefficients?

Views: 1,510

Posted By xTamx420

Reasonable error in lift and drag coefficients?

Hi, I am a new user to Fluent and CFD in general. I have been running simulations on NACA 0012 foils and I was wondering what a reasonable Cd and Cl are? I get around 0.009 for Cd at 0 angle of...

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