Boeing Helicopter, together with other United States helicopter manufacturers, participated in a finite element applications program to emplace in the United States a superior capability to utilize finite element analysis models in support of helicopter airframe design. The activities relating to planning and creating a finite element vibrations model of the Boeing Model 36-0 composite airframe are summarized, along with the subsequent analytical correlation with ground shake test data.


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    Title :

    Plan, formulate, discuss and correlate a NASTRAN finite element vibrations model of the Boeing Model 360 helicopter airframe


    Contributors:
    Gabel, R. (author) / Lang, P. F. (author) / Smith, L. A. (author) / Reed, D. A. (author)

    Publication date :

    1989-04-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English