Comparison of pure helicopter, winged helicopter, tilt-wing propeller VTOL-STOL aircraft, and fixed-wing direct-control STOL aircraft to determine effect of their configuration characteristics on agility performance; maneuvers included horizontal acceleration and deceleration performance, normal load factor capability, turning performance, and attack maneuver that combines decelerating turn with straight-line acceleration; winged helicopter was found to have best agility performance up to its top speed of 180 knots; tilt-wing propeller has best acceleration and normal load factor capability.


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    Titel :

    Agility performance of several V/STOL and STOL aircraft


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Stutz, R.G. (Autor:in) / Price, G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1964


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Agility performance of several vstol and stol aircraft

    PRICE, G. / STUTZ, R. G. | AIAA | 1964



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