Comparison of theoretical and experimental heat transfer on a cooled 20 degrees cone with a laminar boundary layer at a Mach number of 2.02

Richard Scherrer, Forrest E. Gowan
naca-tn-2087
May 1950

Heat-transfer measurements have been made on an air-cooled 20 degree cone with a laminar boundary layer at a Mach number of 2.02. The surface temperature in the instrumented area on the cone was essentially constant at all test conditions; however, this area was preceded by severe surface-temperature gradients.

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