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June 10, 2010, 08:50 |
Airfoil
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#1 |
Senior Member
Join Date: Nov 2009
Posts: 411
Rep Power: 19 |
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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