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|Title: ||Effect of Cooling on Boundary-Layer Stability at Mach Number 3|
|Authors: ||Mack, L.|
|Issue Date: ||1992 |
|Abstract: ||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.|
|Appears in Collections:||JPL TRS 1992+|
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