The use of an uncalibrated cone for determination of flow angles and Mach numbers at supersonic speeds

Morton Cooper, Robert A. Webster
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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