Boeing Helicopters, together with other U.S. Helicopter manufacturers, is engaged in a finite element applications program designed to emplace in the U.S. a superior capability to utilize finite element analysis models in support of helicopter airframe structurel design. This program was given the acronym DAMVIBS (Design Analysis Methods for VIBrationS). The test plan is reviewed and results are presented for a shake test of the Boeing Model 360 helicopter. Results of the test will serve as the basis for validation of a finite element vibration model of the helicopter.


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    Title :

    Ground Shake Test of the Boeing Model 360 Helicopter Airframe


    Contributors:
    Reed, D. A. (author) / Gabel, R. (author)

    Publication date :

    1989-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







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