Internal performance at Mach number to 2.0 of two auxiliary inlets immersed in fuselage boundary layer
1954-03-10
Miscellaneous
No indication
English
Performance of Separation Nose Inlets at Mach Number 5.5
NTRS | 1953
|Aerodynamic and acoustic performance of high Mach number inlets
TIBKAT | 1977
|Noise suppression with high Mach number inlets
TIBKAT | 1976
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