Effect of Thickness, Camber, and Thickness Distribution on Airfoil Characteristics at Mach Numbers up to 1.0
1956-03-01
Miscellaneous
No indication
English
Engineering Index Backfile | 1956
|Effect of Airfoil Thickness, Camber and Reynolds Number on Plunging Airfoil Propulsion
British Library Conference Proceedings | 2009
|