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Please use this identifier to cite or link to this item: http://hdl.handle.net/2014/36709

Title: Effect of Cooling on Boundary-Layer Stability at Mach Number 3
Authors: Mack, L.
Issue Date: 1992
Citation: N/A
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.
URI: http://hdl.handle.net/2014/36709
Appears in Collections:JPL TRS 1992+

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