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Old   July 9, 2009, 04:47
Default supersonic airfoil
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Jules
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Hi every1
I have a project to determine the Cl and Cd for a supersonic airfoil in fluent. only prob is i don't have a airfoil can anyone suggest a supersonic airfoil and where i can get the coordinates.
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Old   July 10, 2009, 11:15
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Hello,

for a supersonic flow you'd better use a rhombic airfoil - for this you also have analytical solutions for M>1.5 .

Check "Modern compressible flow" by J.D.Anderson.

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Old   July 11, 2009, 19:18
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Thanx REnardP
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