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    Title :

    Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow ; Pt. 2: Experimental results for mach numbers 2.00 and 2.58


    Contributors:


    Publication date :

    1966


    Size :

    36 S


    Remarks:

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


    Type of media :

    Report


    Type of material :

    Print


    Language :

    Unknown