This paper describes the calculation of the effect of wall cooling on the instability of a two-dimensional, flat-plate supersonic boundary layer under stratospheric flight conditions at Mach 3 using both the inviscid and viscous linear stability theories.


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    Title :

    Effect of Cooling on Boundary-Layer Stability at Mach Number 3


    Contributors:
    Mack, L. (author)

    Publication date :

    1992-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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