Aerodynamic problems of achieving efficient turbojet exit nozzle installations for operation over wide speed range; particular attention devoted to influence of jet stream interaction on both nozzle thrust and afterbody drag; for this purpose, use is made of shock boundary layer interaction concepts.
Some aerodynamic considerations of nozzle-afterbody combinations
Aeronautical Eng Rev
Aeronautical Engineering Review ; 15 , n 9
1956
7 pages
Aufsatz (Zeitschrift)
Englisch
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