Slender cone boundary layer transition under angle of attack at Mach 21 with promoted leeward and fixed windward ray


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    Title :

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


    Contributors:

    Publication date :

    1971-06-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    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