The Benchmark SuperCritical Wing (BSCW) wind tunnel model served as a semi-blind testcase for the 2012 AIAA Aeroelastic Prediction Workshop (AePW). The BSCW was chosen as a testcase due to its geometric simplicity and flow physics complexity. The data sets examined include unforced system information and forced pitching oscillations. The aerodynamic challenges presented by this AePW testcase include a strong shock that was observed to be unsteady for even the unforced system cases, shock-induced separation and trailing edge separation. The current paper quantifies these characteristics at the AePW test condition and at a suggested benchmarking test condition. General characteristics of the model's behavior are examined for the entire available data set.


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    Titel :

    Experimental Data from the Benchmark SuperCritical Wing Wind Tunnel Test on an Oscillating Turntable


    Beteiligte:
    J. Heeg (Autor:in) / D. J. Piatak (Autor:in)

    Erscheinungsdatum :

    2013


    Format / Umfang :

    25 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Experimental Data from the Benchmark Supercritical Wing Wind Tunnel Test on an Oscillating Turntable

    Heeg, J. / Piatak, D.J. / American Institute of Aeronautics and Astronautics; American Society of Mechanical Engineers; American Society of Civil Engineers | British Library Conference Proceedings | 2013


    Transonic Wind Tunnel Test of Wing Oscillating in Pitch

    Begnini, Guilherme R. / Bones, Carlos A. / Spode, Cleber | AIAA | 2018


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    Begnini, Guilherme R. / Bones, Carlos A. / Spode, Cleber | British Library Conference Proceedings | 2018