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.
Effect of Cooling on Boundary-Layer Stability at Mach Number 3
1992-01-01
Miscellaneous
No indication
English
flight , cooling , stratospheric , boundary , conditions , layer , supersonic , wall
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