This paper examined the wing rock motion of an aircraft model with a configuration of slender fuselage, 81°-swept strake wing, 48°-swept wing and twin vertical tails. These experiments covered the alpha range of 0° to 70° and zero sideslip with a Reynolds number (Re) of 1.2×105.The roll motion pattern can be divided into three regions: No wing rock region (α = 0-20°), micro-vibration region (α = 20°-35° and α = 60°-70°), wing rock region (α = 35°-60°). At the wing rock region, the motion was not induced by asymmetric vortices on slender forebodythrough the analysis of response relationship between wing rock motion and location of nose perturbation.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Wing Rock Motion of an Aircraft Model at Fixed Angle of Attack


    Beteiligte:
    Wang, Y.K. (Autor:in) / Li, Q. (Autor:in) / Shi, W. (Autor:in) / Sun, G.L. (Autor:in)


    Erscheinungsdatum :

    2013


    Format / Umfang :

    10 Seiten, 8 Quellen




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Aircraft Wing Rock in High-Angle-of-Attack Flight

    Ramnath, Rudrapatna V. | AIAA | 2010


    Fixed-wing aircraft rudder deflection angle calibrator

    JIA JUN / YU JIEYONG / FU XIAOMIN et al. | Europäisches Patentamt | 2024

    Freier Zugriff


    Wing and fixed-wing aircraft

    HUANG JINGTAO / MA XIWANG / WANG CHEN'AN et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Micro Fixed-Wing Aircraft Modeling via Motion Tracking

    Minghui, Zhang / Hao, Wang | Springer Verlag | 2025