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
35 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Design of top mounted supersonic inlets for a cylindrical fuselage
SAGE Publications | 2019
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