Preliminary results from a free-flight investigation of boundary-layer transition and heat transfer on a highly polished 8-inch-diameter hemisphere-cylinder at Mach numbers up to 3 and Reynolds numbers based on a length of 1 foot up to 17.7 x 10(exp

Hall, James R Speegle, Katherine C Piland, Robert O
naca-rm-l57d18c
May 16, 1957


No Abstract Available

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