Boundary-layer transition on a cooled 20 degree cone at Mach numbers of 1.5 and 2.0

Richard Scherrer
naca-tn-2131
Jul 1950


The laminar boundary layer on a cooled 20 degree cone was investigated at Mach numbers of 1.5 and 2.0 to determine the variation of the position of transition with surface temperature for both constant surface temperatures and surface temperatures that increased toward the rear of the cone.

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