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Old   June 10, 2010, 08:50
Default Airfoil
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Hello,

I have a (probably) simple problem:

- A wing swept back with 45 degree
- A constant wing section NACA 64A810 normal to the 1/4 chords line

There is any simple formula or program to recover the wing section parallel with the symmetry plane ?

I was thinking to create a "cylinder" using the NACA section and intersect this with a plane at 45 degree, the intersection curve should be my searched airfoil.

Any other suggestions will be appreciated.

Thanks,

Do
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