Conical shock wave-turbulent boundary layer interaction data obtained for adiabatic wall conditions at supersonic free stream Mach numbers, including suction effects


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    Title :

    Conical shock-wave turbulent boundary-layer interaction including suction effects


    Contributors:

    Conference:

    AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 5TH, U.S. AIR FORCE ACADEMY ; 1969 ; COLORADO SPRINGS, CO


    Publication date :

    1970-08-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English