The paper describes and analyses potential concepts for gust alleviation at transonic speeds applied on a forward swept transport aircraft configuration. The main objective is to reduce structural weight by minimizing gust induced loads. Both inviscid and viscous aerodynamic simulations are performed for analysis. A gust study reveals a critical gust wave length of 50m leading to highest aerodynamic loads at cruise conditions. Gust induced separation is observed for particular cases. Deflection of a wing tip flap and the aileron at the outer wing have a remarkable short response time and offer strong flow actuation to reduce gust loads.


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    Titel :

    Gust Alleviation on a Forward Swept Wing Transport Aircraft


    Beteiligte:
    Klug, L. (Autor:in) / Heinrich, R. (Autor:in) / Streit, T. (Autor:in) / Radespiel, R. (Autor:in)

    Erscheinungsdatum :

    2021


    Format / Umfang :

    6 pages



    Medientyp :

    Sonstige


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Schlagwörter :


    Gust Alleviation on a Forward Swept Transport Aircraft at Transonic Speeds

    Radespiel, Rolf / Wild, Jochen / Heinrich, Ralf et al. | AIAA | 2021


    GUST ALLEVIATION ON A FORWARD SWEPT TRANSPORT AIRCRAFT AT TRANSONIC SPEEDS

    Radespiel, Rolf / Wild, Jochen / Heinrich, Ralf et al. | TIBKAT | 2021


    Gust alleviation by spanwise load control applied on a forward and backward swept wing

    Klug, L. / Ullah, J. / Lutz, T. et al. | Springer Verlag | 2023

    Freier Zugriff


    INVESTIGATION OF GUST LOADS ON A FLEXIBLE FORWARD SWEPT WING

    Handojo, V. / Meddaikar, Y. M. / Dillinger, J. K. S. et al. | TIBKAT | 2020