In order to provide information for flutter and dynamic stress calculations on aircraft, knowledge of normal modes of vibration is required; matrix method, due to Dr. TRAILL-NASH, is extended and used to obtain general expression for complete aircraft normal modes, and is applicable to most aircraft configurations; method is considered eminently suitable for use with modern digital electronic computational equipment.


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    Title :

    Normal modes of vibration of aircraft


    Additional title:

    Aircraft Eng


    Contributors:
    Shevloff, N.P. (author) / Reid, T.J. (author)

    Published in:

    Publication date :

    1953


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    The Normal Modes of Vibration of an Aircraft

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