[hat3744]

Dear all,

I desire to use the FLUENT to calculate the aerodynamic loads on the 2-D airfoil with flap track fairing.
On design point, it will fly at 35,000 feet with Mach 0.82 (around 300 knots). Because this part is not only the conventional airfoil, but also attachs the flap track fairing rearward,
(refer to: http://www.facebook.com/album.php?ai...&id=1074041340)

1. How can I define the Re? (where it's not the conventional airfoil)
2. Which type of mesh is suitable for it?
3. Which Turbulent Modeling, in Fluent, is suitable for it?
4. Do I have to setup any more details to complete it?

Thank you very much for your attention.
Best Regards,
Hat3744