supersonic airfoil
 

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 :)

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

Thanx REnardP
:)