Internal performance at Mach number to 2.0 of two auxiliary inlets immersed in fuselage boundary layer
10.03.1954
Sonstige
Keine Angabe
Englisch
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
|