This paper presents the results of an analytical study aimed at predicting the aeromechanical stability of a helicopter in ground resonance, with the inclusions of aerodynamic forces. The theoretical results are found to be in good agreement with the experimental results, available in the literature, indicating that the coupled rotor/fuselage system can be represented by a reasonably simple mathmatical model.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Coupled helicopter rotor/body aeromechanical stability comparison of theoretical and experimental results


    Beteiligte:
    Friedmann, P. P. (Autor:in) / Venkatesan, C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.02.1985



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch







    Influence of Balanced Rotor Anisotropy on Helicopter Aeromechanical Stability

    Gandhi, F. / Malovrh, B. / American Helicopter Society | British Library Conference Proceedings | 1997


    Aeromechanical Stability of a Bearingless Rotor Helicopter with Double-Swept Blades

    Zhang, Junhao / Xia, Pinqi / Chopra, Inderjit | AIAA | 2021

    Freier Zugriff