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Forum: FLUENT

October 10, 2012, 22:49

Replies: 8

CFD Analysis of Airfoil at Mach = 0.0

Views: 1,852

Posted By Hybrid

Flow is incompressible (M < 0.3), So what will be...

Flow is incompressible (M < 0.3), So what will be the velocity then for M=0.0.

Forum: FLUENT

October 8, 2012, 04:39

Replies: 8

CFD Analysis of Airfoil at Mach = 0.0

Views: 1,852

Posted By Hybrid

CFD Analysis of Airfoil at Mach = 0.0

Hi folks

I want to perform a 2-D airfoil CFD analysis at Reynolds number of 9.0M and Mach number 0.0.

Is this possible?

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