Study of impact of mixed mission requirements for tactical and strategic aircraft on inlet design and inlet engine interaction; missions include subsonic high altitude, transonic low altitude, and supersonic high altitude flight conditions; inlet-engine airflow matching, inlet drag, inlet weight, and their effects on vehicle weight and drag characteristics may be far more important measures of integrated performance than inlet pressure recovery; influence of vehicle-inlet flow field interactions, maneuvering conditions, and off-design inlet conditions on inlet-engine stability and performance are discussed; for V/STOL tactical aircraft, inlet requirements for takeoff, transition and high speed flight and effect of hot gas reingestion on inlet-engine compatibility are presented.
Airframe-propulsion integration for future aircraft systems
SAE -- Paper
SAE Meeting ; 1968
1968
20 pages
Aufsatz (Konferenz)
Englisch
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Airframe-Propulsion Integration for Future Aircraft Systems
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