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

    Publication date :

    1989


    Size :

    296 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English