The objectives of this study were to verify the accuracy of the hybrid computer version of the Rotorcraft Simulation Program C81 as a flapping predictor, to investigate the effect of operational envelope limits on flapping, and to investigate methods of extending the recommended operational envelopes of the subject helicopter.


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    Title :

    Effect of Operational Envelope Limits on Teetering Rotor Flapping


    Contributors:

    Publication date :

    1978


    Size :

    94 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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