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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    Titel :

    Finite Element Modeling of the Higher Harmonic Controlled OH-6A Helicopter Airframe


    Beteiligte:
    D. Ferg (Autor:in) / M. Toossi (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    66 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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