Morton Cooper, Robert A. Webster
naca-tn-2190
Mar 1951
A pressure-distribution investigation of a body revolution has been conducted in the Langley 4- by 4-foot supersonic tunnel at a Mach number of 1.59 and a Reynolds number of 1.04 X 10 to the sixth power per foot.
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http://naca.central.cranfield.ac.uk/reports/1951/naca-tn-2190.pdf