A STOL medium tactical transport featuring 1000 ft takeoff distance performance has been established utilizing the powered-lift wing to achieve STOL capability. Two powered-lift wing concepts, the augmented jet flap and the externally blown flap, are presented as optimum for a minimum thrust-to-weight ratio configuration. Interconnecting the propulsion system with engine cross ducting minimizes the unsymmetrical lift resulting from an engine failure. A commercial counterpart to the military transport is discussed.


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    Titel :

    Propulsion System Impact on Military/Commercial STOL Transport Commonality


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Stalder, J. P. (Autor:in)

    Kongress:

    National Air Transportation Meeting ; 1970



    Erscheinungsdatum :

    01.02.1970




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    MILITARY/COMMERCIAL STOL TRANSPORT COMMONALITY

    KLECKNER, HAROLD F. | SAE Technical Papers | 1971




    Prospects for commercial commonality in military transports

    BARBER, E. / MARHEFKA, R. / BLATTNER, D. | AIAA | 1978