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    Title :

    Low-speed wind-tunnel tests on a unswept wing-fuselage model of aspect ratio 9.8, with tangential blowing over trailing-edge flaps and ailerons, including the effect of slipstream


    Contributors:


    Publication date :

    1970


    Size :

    21 S., [18] Bl.


    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 :

    English