Flow Studies in the Asymmetric Adjustable Nozzle of the Ames 6-by 6-foot Supersonic Wind Tunnel
1949-09-15
Miscellaneous
No indication
English
Asymmetric adjustable supersonic nozzle for wind-tunnel application
Engineering Index Backfile | 1953
|Supersonic Retropropulsion Experimental Results from NASA Ames 9 × 7 Foot Supersonic Wind Tunnel
Online Contents | 2014
|