An MSC/NASTRAN finite element model of the higher harmonic control configured OH-6A helicopter fuselage was developed. This finite element model was verified by performing various model checkouts and correlation with results from a ground vibration test.


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    Title :

    Finite element modeling of the higher harmonic controlled OH-6A helicopter airframe


    Contributors:

    Publication date :

    1990-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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