Paper describes digital program structure input data used, and results produced; complete blade element analyses of main rotor, tail rotor, and propellers are performed throughout maneuver based on instantaneous aerodynamic and dynamic environment; time histories of main rotor blade loads and bending moments are calculated; examples of cases studied, including full autorotative landing, and high-performance deceleration using reversed propeller thrust.


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    Titel :

    Computer flight testing of rotorcraft


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Duhon, J.M. (Autor:in) / Harvey, K.W. (Autor:in) / Blankenship, B.L. (Autor:in)


    Erscheinungsdatum :

    1965


    Format / Umfang :

    13 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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