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Forum: Main CFD Forum

June 16, 2010, 11:06

Replies: 3

Airfoil

Views: 1,837

Posted By DoHander

Thanks, however I've solved the problem in...

Thanks,

however I've solved the problem in two ways:

1. I've used a parametric model of my wing in Rhinoceros (a demo version).
2. I've found an exact analytical solution to my problem tested...

Forum: Main CFD Forum

June 10, 2010, 08:50

Replies: 3

Airfoil

Views: 1,837

Posted By DoHander

Airfoil

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...

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