Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Performance characteristics at Mach numbers to 2.0 of various types of side inlets mounted on fuselage of proposed supersonic airplane : IV. Rectangular-cowl inlets with two-dimensional compression ramps


    Contributors:


    Publication date :

    1952


    Size :

    35 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