Theoretically there is large thrust gain available by efficiently expanding exhaust gases at high aircraft speeds; methods of expanding exhaust by means of convergent-divergent nozzles; variable convergent-divergent nozzles, and ejector nozzles; typical installations; schematics and thrust increase curves; matching of air intakes and nozzles.
Exhaust nozzles for supersonic aircraft
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 62 , n 573
1958
5 pages
Aufsatz (Zeitschrift)
Englisch
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