A new wind tunnel environment for low Reynolds number testing of Micro Air Vehicles (MAV) is introduced, providing a test rig for plunge and pitch motions and a 6-component force balance. In this study a rigid as well as a flexible version of a typical MAV wing is investigated. Optical measurements techniques are adapted to measure simultaneously the instantaneous model position, orientation, wing deformations and flow fields.


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    Titel :

    Simultaneous Measurements of Unsteady Aerodynamic Loads, Flow Velocity Fields, Position and Wing Deformations of MAVs in Plunging Motion


    Beteiligte:
    Konrath, R. (Autor:in) / Schlager, B. (Autor:in) / Kirmse, T. (Autor:in) / Kompenhans, J. (Autor:in) / Möller, T.J. (Autor:in) / Wokoeck, R. (Autor:in) / Emge, M. (Autor:in) / Radespiel, R. (Autor:in)


    Erscheinungsdatum :

    2010


    Format / Umfang :

    8 Seiten





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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