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.


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    Titel :

    Airframe-propulsion integration for future aircraft systems


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Richey, G.K. (Autor:in) / Stava, D.J. (Autor:in) / Brimelow, B. (Autor:in) / Bush, H.I. (Autor:in)

    Kongress:

    SAE Meeting ; 1968



    Erscheinungsdatum :

    1968


    Format / Umfang :

    20 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Airframe-Propulsion Integration for Future Aircraft Systems

    Brimelow, B. / Stava, D. J. / Richey, G. K. et al. | SAE Technical Papers | 1968


    Airframe-Propulsion Integration for Fighter Aircraft

    RICHEY, G.K. / SURBER, L.E. / BERRIER, B.L. | AIAA | 1983


    Propulsion/airframe integration issues for waverider aircraft

    Blankson, Isaiah M. / Hagseth, Paul | NTRS | 1993


    Propulsion/airframe integration issues for waverider aircraft

    BLANKSON, ISAIAH / HAGSETH, PAUL | AIAA | 1993


    Propulsion airframe integration

    Mikkelson, D. | NTRS | 1975