Minimum takeoff and landing distances are calculated for 2 overloaded, propeller driven, tilt wing VTOL aircraft; effects of flap setting, propeller thrust variation with forward speed, runway surface, wing tilt rate and flap boundary layer control are considered at various thrust to weight ratios; it appears that takeoff to landing from 50-ft obstacle can be achieved in 500 ft at all-up-weight (AUW) between 40% and 50% greater than VTO AUW, depending on assumed thrust variation with forward speed.


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    Titel :

    Field requirements of overloaded propeller-driven VTOL aircraft


    Weitere Titelangaben:

    Can Aeronautics Space J


    Beteiligte:
    Neal, B. (Autor:in) / Lyster, H.N.C. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :