The ground effect on flapping wing is investigated numerically based on the immersed boundary-lattice Boltzmann method. A NACA0012 airfoil is considered in this work. The airfoil executes oscillation along vertical direction near ground. The simulations have been carried out for some parameters including the distance between the foil and the ground and frequency of oscillation as well. The ground effect on the force behaviors and vortex structures is analyzed. The results achieved in this work can shed physical insight into the understanding of aerodynamics and flow structures for air vehicle flying near the ground or water surface.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Ground Effect on Flapping Wing


    Beteiligte:
    Wu, J. (Autor:in) / Zhao, N. (Autor:in)


    Erscheinungsdatum :

    2013


    Format / Umfang :

    8 Seiten, 14 Quellen




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Ground effect wing having a flapping wingtip

    KAREM ABRAHAM / PARCELL JOHN PAUL | Europäisches Patentamt | 2023

    Freier Zugriff

    Four-wing flapping wing mechanism with four-flapping effect

    XIE PENG / XIONG MINWEN / HUANG YALONG | Europäisches Patentamt | 2023

    Freier Zugriff

    Flat-flapping-wing flapping-wing aircraft

    WANG ZHICHENG | Europäisches Patentamt | 2015

    Freier Zugriff

    Flow structures around a flapping wing considering ground effect

    Truong, Tien Van / Kim, Jihoon / Kim, Min-Jun et al. | Tema Archiv | 2013


    Four-wing flat-flapping flapping-wing aircraft

    WANG ZHICHENG | Europäisches Patentamt | 2015

    Freier Zugriff