The report presents the analysis of 728 hours of testing, conducted in the Boeing V/STOL 20 x 20 ft. Wind Tunnel, on a model of a medium STOL transport with vectored thrust and jet flap powered-lift systems. The interactions between the two powered lift systems and the basic airplane aerodynamics are presented for a systematic series of configuration changes which include sweep and nacelle location. (Modified author abstract)


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    Titel :

    STOL Tactical Aircraft Investigation. Volume IV. Analysis of Wind Tunnel Data: Vectored Thrust/Mechanical Flaps and Internally Blown Jet Flaps


    Beteiligte:
    J. R. Monk (Autor:in) / J. L. Lee (Autor:in) / J. P. Palmer (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    305 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch