Theory presented of ejector nozzle in which secondary shroud is cylindrical, which is based on continuity, momentum and maximizing of secondary flow; good agreement with experiment obtained.
Theory of cylindrical ejector supersonic propelling nozzle
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 62 , n 574
1958
6 pages
Aufsatz (Zeitschrift)
Englisch
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