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    Title :

    Experimental flowfield visualization of a high alpha wing at Mach 1.62


    Author / Creator :

    PITTMAN, JAMES L.


    Contributors:

    Published in:

    Journal of Aircraft ; 24 , 5 ; 335-341


    Publication date :

    1987




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    Body and canard effects on an attached-flow maneuver wing at Mach 1.62

    Pittman, J. L. / Miller, D. S. / Mason, W. H. | NTRS | 1984


    Body and Canard Effects on an Attached-Flow Maneuver Wing at Mach 1.62

    J. L. Pittman / D. S. Miller / W. H. Mason | NTIS | 1984


    Turbulent-heat-transfer measurements at mach number of 1.62

    Brevoort, M.J. / Rashis, B. | Engineering Index Backfile | 1955