Aircraft and missile structural vibration problems, and dynamics problems associated with missile test and launch equipment may be represented ideally by masses interconnected by extensional and rotational springs; method enabling engineer rapidly to set up vibration problems by using electronic computer and by filling primary data into basic matric equation.


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    Title :

    Matric formulation of linearly coupled vibration problems


    Additional title:

    Aircraft Eng


    Contributors:
    Cox, H.L. (author)

    Published in:

    Publication date :

    1958


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    A Matric Formulation of Linearly Coupled Vibration Problems

    Cox, Hugh L. | Emerald Group Publishing | 1958


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