The overall objective of the design effort was to conduct a preliminary vehicle-sizing activity to establish baseline configurations for the STOL tactical aircraft investigation. These preliminary baselines were used for the takeoff and landing studies and as a point of departure for wind tunnel test planning and flight control technology activities. The lift/propulsion concepts studied were: Externally Blown Flap (EBF); Mechanical Flap plus Vectored Thrust (MF/VT); and Internally Blown Flap (IBF). The report summarizes the design activities for the three-month and six-month configuration reviews.


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    Titel :

    STOL Tactical Aircraft Investigation. Volume I. Configuration Definition


    Beteiligte:
    J. Hebert (Autor:in) / C. Whitney (Autor:in) / R. E. Johnston (Autor:in) / G. B. Nicoloff (Autor:in) / E. C. Laudeman (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    169 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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