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    Title :

    Application of shock tubes to transonic airfoil testing at high reynolds numbers


    Contributors:

    Published in:

    Publication date :

    1978


    Size :

    VI, 63 S


    Remarks:

    Ill., graph. Darst
    Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek


    Type of media :

    Book


    Type of material :

    Print


    Language :

    Unknown




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    Transonic unsteady pressure measurements on a supercritical airfoil at high Reynolds numbers

    HESS, ROBERT W. / SEIDEL, DAVID A. / IGOE, WILLIAM B. et al. | AIAA | 1989


    Shock Tube as a Device for Testing Transonic Airfoils at High Reynolds Numbers

    William J. Cook / Leroy L. Presley / Gary T. Chapman | AIAA | 1979