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    Title :

    Supercritical airfoil drag reduction by passive shock wave/boundary layer control in the Mach number range .75 to .90


    Contributors:
    NAGAMATSU, H. (author) / FICARRA, R. (author)

    Conference:

    23rd Aerospace Sciences Meeting ; 1985 ; Reno , NV , U.S.A.



    Publication date :

    1985-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English