Reversible morphing wings, which can exchange the leading and trailing edges, expand architectural possibilities for aerial robotics (e.g., stopped-rotor configurations). However, few designs are scaled for uncrewed aerial vehicle (UAV) applications or effectively address the coupled aerodynamic and structural challenges of morphing. As such, we present a novel reversible wing design that uses rigid parallelogram slats mounted on a flexible substrate, creating a compliant yet aerodynamically robust structure. One-way fluid-structure interaction simulations validate the wing's structural performance under airflow. Compared to other reversed-flow wings, the proposed configuration doubles reverse-flow performance relative to a Clark-Y wing and improves upon the 0° angle of attack performance compared to other reversible morphing wings.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Slat-Inspired Reversible Wing for Stopped-Rotor Vehicles


    Beteiligte:
    Hilby, Kristan (Autor:in) / Hughes, Max (Autor:in) / Hunter, Ian (Autor:in)


    Erscheinungsdatum :

    14.05.2025


    Format / Umfang :

    3505710 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Flywheel Rotor/Wing Makes Stopped Rotor Aircraft Practical

    Pande, J. B. / American Helicopter Society | British Library Conference Proceedings | 1999


    Slat for an aircraft wing

    DENYS CUSTANCE | Europäisches Patentamt | 2020

    Freier Zugriff

    Low noise wing slat system with rigid cove-filled slat

    Shmilovich, Arvin / Yadlin, Yoram | NTRS | 2013


    Slat for an aircraft wing

    DENYS CUSTANCE | Europäisches Patentamt | 2020

    Freier Zugriff