Performance Characteristics at Mach Numbers to 2.0 of Various Types of Side Inlets Mounted on Fuselage of Proposed Supersonic Airplane I : Two-dimensional Compression-ramp Inlets with Semicircular Cowls
16.07.1952
Sonstige
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Englisch
Design of top mounted supersonic inlets for a cylindrical fuselage
SAGE Publications | 2019
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