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    Title :

    High-speed tunnel tests of a 5 per cent. chord dive-recovery flap on a NACA 0015 aerofoil


    Contributors:


    Publication date :

    1953


    Size :

    19 S.


    Remarks:

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


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik