Based on studies of aerodynamic and control requirements of VTOL aircraft and experience gained from installation of propellers on tail sitter Lockheed XFV-1 and Convair XFY-1 aircraft, it appeared that propeller driven VTOL aircraft could be designed with required performance and flying characteristics; optimum vehicle should have wing designed to operate at lift coefficient for maximum lift/drag ratio to obtain peak cruise performance; results of experiments on X-100 and M200 aircraft.


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    Titel :

    High-speed VTOL X-100 and M200 aircraft


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:
    Borst, H.V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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