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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 :

    1955-08-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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

    Dunning, R.W. / Ulmann, E.F. | Engineering Index Backfile | 1955



    Pressure Measurements on an Ogive-cylinder Body at Mach Number 4.04

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


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

    Ulmann, Edward F. / Lord, Douglas R. | NTRS | 1950