A variety of aircraft morphing technologies have been investigated and represented by various researchers in the public domain. The morphing wing concepts involved the modification of aircraft wings during the in-flight course. Most of the technologies/concepts were based on biomimicry, where wing aerodynamic performance improved due to the change in wing shape. Here we describe a novel concept where in the flow parameters of airfoils arranged in configurations are investigated. The flow parameters are investigated using the numerical simulation tool ANSYS. A 2d flow simulation is performed using a Fluent solver to evaluate the flow configuration of the airfoils arranged in different configurations. The first configuration of airfoils is named a base, wherein the airfoils are arranged at zero angles of attack. The other two configurations are arranged by increasing the angular position of airfoils i.e., 15, 30, and 45 degrees. All these configurations are aerodynamically investigated at different sub-sonic speeds.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Gliding Analysis of Segmented Flapping Wing


    Beteiligte:
    Govardhan D. (Autor:in) / Kameswara Surya Teja K. (Autor:in) / Jayahari L. (Autor:in)


    Erscheinungsdatum :

    2024




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt





    Flapping wing-gliding composite micro-aircraft and controllable gliding control method thereof

    WU YULIE / XIAO DINGBANG / WU XUEZHONG et al. | Europäisches Patentamt | 2024

    Freier Zugriff


    Hovering and gliding multi-wing flapping micro aerial vehicle

    RATTI JAYANT / JONES EMANUEL / VACHTSEVANOS GEORGE | Europäisches Patentamt | 2016

    Freier Zugriff

    Bionic aircraft torsion flapping wing structure with gliding function

    DU QIANG / XUE SHIQIN / WANG NA et al. | Europäisches Patentamt | 2024

    Freier Zugriff