The Stalled Airfoil Analysis Program (SAAP) is a computer code for predicting the aerodynamic characteristics of an airfoil up to, and beyond, stall. SAAP is presently evaluated through comparisons with experiments and with two other theoretical methods over an extensive range of airfoils and Reynolds number conditions. SAAP modeled drag more accurately than either of the other methods, and at angles of attack below stall yielded a smoother lift variation with angle of attack.
Evaluation of a stalled airfoil analysis program
Journal of Aircraft ; 22
1985-02-01
Sonstige
Keine Angabe
Englisch
Evaluation of a stalled airfoil analysis program
AIAA | 1985
|Transitory Separation Control Over a Stalled Airfoil
British Library Conference Proceedings | 2009
|Transitory Separation Control Over a Stalled Airfoil
AIAA | 2009
|