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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

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


    Beteiligte:
    Ferg, Douglas (Autor:in) / Toossi, Mostafa (Autor:in)

    Erscheinungsdatum :

    01.10.1990


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Improved Finite Element Modeling of Helicopter Airframe Connections

    Yun, S. / Lemnios, A. / Bacchau, O. et al. | British Library Conference Proceedings | 1997


    Helicopter airframe

    FINK AXEL / STEINDL CHRISTOPH | Europäisches Patentamt | 2018

    Freier Zugriff

    Helicopter Airframe Fatigue Spectra Generation

    Krake, Luther | Trans Tech Publications | 2014


    Helicopter Airframe Fatigue Spectra Generation

    Krake, Luther | Tema Archiv | 2014