Data, of interest to airplane designers, on flutter and vibration of structures to which control surfaces are attached; this source of danger may be controlled; modern methods of stress analyses and load factors in current use are adequate to provide all strength needed in airplane structures for flight in rough air, and for all necessary maneuvers. Before Int Automotive Eng Congress.


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    Title :

    Airplane vibrations and flutter controllable by design


    Additional title:

    Soc Automotive Engrs J


    Contributors:
    Roche, J.A. (author)


    Publication date :

    1933


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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