Subsonic air intake, Mach 2 transport aircraft intake, and Mach 3 are considered. Hypersonic cruise intakes are mentioned. The problem of supersonic intake adaptation to the intermediate flight Mach number range is reviewed. Future multicycle engine design is discussed.
Transport Aircraft Intake Design
1988
28 pages
Report
Keine Angabe
Englisch
Design and development of air intake for supersonic transport aircraft
Engineering Index Backfile | 1968
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