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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    Title :

    Computer flight testing of rotorcraft


    Additional title:

    Am Helicopter Soc -- J


    Contributors:


    Publication date :

    1965


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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