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    Title :

    Effects of sweep and angle of attack on boundary-layer transition on wings at Mach number 4.04


    Contributors:


    Publication date :

    1955


    Size :

    31 S


    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




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    Lord, Douglas R / Ulmann, Edward F | NTRS | 1952


    Tests of a Hermes A-2 Missile Body at Mach Number 4.04

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