Performance Characteristics at Mach Numbers to 2.0 of Various Types of Side Inlets Mounted on Fuselage of Proposed Supersonic Airplane IV : Rectangular Cowl Inlets with Two-dimensional Compression Ramps
1952-10-28
Sonstige
Keine Angabe
Englisch
Design of top mounted supersonic inlets for a cylindrical fuselage
SAGE Publications | 2019
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