Aerodynamic design of high contraction ratio, subsonic wind tunnel inlets
22nd Aerospace Sciences Meeting ; 1984 ; Reno , NV , U.S.A.
1984-01-01
Conference paper
Electronic Resource
English
Starting Mechanisms for High Contraction Ratio Hypersonic Inlets
British Library Conference Proceedings | 2011
|Subsonic Scarf Inlets Investigated
NTRS | 2005
|