This code provides the variation of CL, CD and CM with angle of attack of a
symmetrical double wedge airfoil. Additionally it provides the coefficient of
pressure variation at a requested angle of attack on the surface of the airfoil.
The user can provide the geometry and free stream condition to carryout
Upload date : 2015-11-23 20:23:48
MD5 : 994a20584f417686265a4140c87d2fbf
SHA1 : a67fdfd57da2c81f8883f0e5330f63dfd4015438
Downloads : 801