Tests of a Triangular Wing of Aspect Ratio 2 in the Ames 12-foot Pressure Wind Tunnel I : the Effect of Reynolds Number and Mach Number on the Aerodynamic Characteristics of the Wing with Flap Undeflected
1948-01-22
Miscellaneous
No indication
English
Flexible High Aspect Ratio Wing Wind Tunnel Tests
TIBKAT | 2023
|Flexible High Aspect Ratio Wing Wind Tunnel Tests
AIAA | 2023
|