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    Title :

    Effect of angle of attack on boundary-layer transition at Mach 21


    Author / Creator :

    FISCHER, M. C., RUDY, D. H. /NASA, LANGLEY RESEARCH CENTER, HYPERSONIC VEHICLES DIV., HAMPTON, VA./.


    Contributors:

    Published in:

    AIAA Journal ; 9 , 6 ; 1203-1205


    Publication date :

    1971




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English






    BOUNDARY-LAYER TRANSITION ON CONES AT ANGLE OF ATTACK IN A MACH-6 QUIET TUNNEL

    Swanson, E. / Schneider, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010