Attempt made to correlate theoretically calculated decay effects of wing oscillations at subcritical flutter speeds with results obtained during actual flight flutter testing at these speeds; theory discussed gives reasonably good agreement with limited number of test data obtained in flight from single airplane.


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    Title :

    Note on flight flutter testing


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1948


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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