Considerable research on large-scale high-performance, lift-engine, V/STOL configurations was conducted at Ames Research Center; exhaust gas reingestion characteristics, lift-engine inlet total-pressure recovery and distortion, and engine-airframe induced effects were measured in 40×80-ft wind tunnel both in and out of ground effects over wide range of transition flight conditions; results show that lift-engine configurations studied may have severe operational constraints placed upon them during transition. (06461)
Low-speed characteristics of high-performance lift-engine V/STOL aircraft
SAE Paper
SAE Meeting ; 1968 VTOL-STOL
1968
10 pages
Aufsatz (Konferenz)
Englisch
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