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July 9, 2009, 04:47
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supersonic airfoil
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#1 |
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New Member
Jules
Join Date: Jul 2009
Location: Sydney, Australia
Posts: 9
Rep Power: 16  |
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. Thanx Jules
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July 10, 2009, 11:15
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#2 |
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Member
Join Date: Mar 2009
Posts: 62
Rep Power: 17 |
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. RenardP |
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July 11, 2009, 19:18
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#3 |
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New Member
Jules
Join Date: Jul 2009
Location: Sydney, Australia
Posts: 9
Rep Power: 16 |
Thanx REnardP
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