Internal performance at Mach number to 2.0 of two auxiliary inlets immersed in fuselage boundary layer
10.03.1954
Sonstige
Keine Angabe
Englisch
Aerodynamic and acoustic performance of high Mach number inlets
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|Performance of Separation Nose Inlets at Mach Number 5.5
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|Noise suppression with high Mach number inlets
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