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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    Titel :

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


    Beteiligte:
    Mack, L. (Autor:in)

    Erscheinungsdatum :

    01.01.1992


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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