Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings incorporating leading edge camber as influenced by Reynolds numbers up to 8.00 x 10(exp 6) and Mach numbers up to 0.29
06.10.1955
Sonstige
Keine Angabe
Englisch
Leading Edge Flaps at Low Reynolds Numbers
AIAA | 2008
|Leading Edge Flaps at Low Reynolds Numbers
British Library Conference Proceedings | 2008
|