Preliminary heat-transfer studies on two bodies of revolution at angle of attack at a Mach number of 3.12

Norman Sands, John R. Jack
naca-tn-4378
Sep 1958


Local rates of heat transfer were obtained for a cone-cylinder model and a parabolic-nosed-cylinder model at a Mach number of 3.12 and angles of attack up to 18 degrees. Data were obtained for cooled surfaces at unit Reynolds numbers of 0.36 and 0.65 million per inch based on free-stream conditions. Zero angle of attack data are included for comparison.

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