Study establishes distribution function of peak response values, based on frequency interpretation. Excitations considered include impact loading on landing gears and aircraft gust loading. Because of relative severity of excitations, prediction of fatigue and maximum response characteristics is important part of task of structural analysis and design.


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    Title :

    Peak structural response to nonstationary random excitations


    Contributors:
    Shinozuka, M. (author) / Yang, J.-N. (author)

    Publication date :

    1971-06-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :