http://www58.wolframalpha.com/input/?i=NACA+2412+airfoil%2C+12deg
See NACA 2412 at AoA 12 degs...you get the lift coefficient and critical mach number.
2009-05-21
Subscribe to:
Post Comments (Atom)
A4 AVIATION WORX concentrates in energy efficient designs
No comments:
Post a Comment