A coupled model of aeroelasticity and flight dynamics for high-altitude, long-endurance (HALE) aircraft is under development based on the geometrically exact, fully intrinsic beam theory, ONERA aerodynamic stall model, and six degrees of freedom model of rigid body motion. The correlation among the present model, MSC/Nastran, UM/NAST, and NATASHA was studied, including the cases of static equilibrium and forced vibration of a split beam system and trim of a Flying-Wing aircraft. The preliminary validation indicates that the present model is effective in modeling a split beam system and the trim of HALE aircraft.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Preliminary validation of a coupled model of nonlinear aeroelasticity and flight dynamics for HALE aircraft


    Beteiligte:
    Jian Zhang, (Autor:in) / Jinwu Xiang, (Autor:in)


    Erscheinungsdatum :

    01.06.2010


    Format / Umfang :

    980520 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Nonlinear Aeroelasticity of Flexible Wing Structure Coupled with Aircraft Flight Dynamics

    Nguyen, Nhan / Trinh, Khanh / Nguyen, Daniel et al. | AIAA | 2012


    Nonlinear Aeroelasticity of Flexible Wing Structure Coupled with Aircraft Flight Dynamics

    Nguyen, N. / Trinh, K. / Nguyen, D. et al. | British Library Conference Proceedings | 2012



    Coupled Aeroelasticity and Flight Dynamics of Active Morphing Aircraft

    Soneda, Kensuke / Tsushima, Natsuki / Yokozeki, Tomohiro et al. | TIBKAT | 2023


    Coupled Aeroelasticity and Flight Dynamics of Active Morphing Aircraft

    Soneda, Kensuke / Tsushima, Natsuki / Yokozeki, Tomohiro et al. | AIAA | 2023