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
28.10.1952
Sonstige
Keine Angabe
Englisch
Design of top mounted supersonic inlets for a cylindrical fuselage
SAGE Publications | 2019
|