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    Title :

    Investigation of the effects of twist and camber on the aerodynamic characteristics of a 50 [degrees] 38' sweptback wing of aspect ratio 2.98 : transonic-bump method


    Contributors:


    Publication date :

    1951


    Size :

    30 S


    Remarks:

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


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English