A modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for the effects of thickness on the lift distribution
1951-02-01
Miscellaneous
No indication
English
AIRFOILS, CAMBERED , AIRFOILS - NACA 631 012 - CHARACTERISTICS , LIFT DISTRIBUTION - AIRFOILS , THEORIES - AIRFOILS, THIN , AIRFOILS - NACA 64A810 (A=0 8) (MOD ) - CHARACTERISTICS , AIRFOILS - NACA 0010-63 (C1I=0 8) (MOD ) (A=0 8) - CHARACTERISTICS , AIRFOILS - THICKNESS , VORTICES - AIRFOILS , AIRFOILS - NACA 0018 - CHARACTERISTICS , ANGLE OF ATTACK
Engineering Index Backfile | 1951
|Calculation of airfoil section with arbitrary pressure distribution
Engineering Index Backfile | 1938
|General theory of airfoil sections having arbitrary shape or pressure distribution
Engineering Index Backfile | 1945
|