Mach 5 aerodynamic coefficients for a hypersonic experimental airplane are examined at JAXA 0.5m hypersonic wind tunnel. 6 DOF forces the model are measured and evaluated. CFD analyses for the same airframe are performed simulating real flight condition for the experimental airplane. As a result, variations of aerodynamic coefficients on angle of attack for both wind tunnel test and CFD analysis are consistent in general.


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    Titel :

    Mach 5 Wind Tunnel Test of Hypersonic Airplane


    Beteiligte:
    H. Taguchi (Autor:in) / K. Fujita (Autor:in) / S. Shindo (Autor:in) / S. Tsuda (Autor:in) / N. Hirabayashi (Autor:in)

    Erscheinungsdatum :

    2007


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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