Several static and dynamic forced-motion wind-tunnel tests on a generic unmanned combat air vehicle configuration with a 53 deg swept leading edge are reviewed. The static tests include both subsonic and transonic measurements. These tests are part of an international research effort to assess and advance the state-of-the-art of computational-fluid-dynamics methods to predict the static and dynamic stability and control characteristics for this type of configuration. The tests included analysis of trailing-edge control surface effectiveness. This paper describes the data collected from three different models of this unmanned combat air vehicle configuration in four different wind tunnels. A subset of this large experimental dataset was selected as focus test cases for computational-fluid-dynamics comparison. The focus test case data are presented in detail.


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    Titel :

    Experimental Investigations of a Generic Swept Unmanned Combat Air Vehicle with Controls


    Beteiligte:
    Vicroy, Dan D. (Autor:in) / Huber, Kerstin C. (Autor:in) / Schütte, Andreas (Autor:in) / Rein, Martin (Autor:in) / Irving, Jonathan P. (Autor:in) / Rigby, Glyn (Autor:in) / Löser, Thomas (Autor:in) / Hübner, Andreas-René (Autor:in) / Birch, Trevor J. (Autor:in)

    Erschienen in:

    Journal of Aircraft ; 55 , 2 ; 475-501


    Erscheinungsdatum :

    2016-07-25


    Format / Umfang :

    27 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch