Measurements Of The Static Pressure Distributions And Shock Shape On An Oblate Spheroid At Mach Numbers Of 3 And 6
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Measurements of the Static Pressure Distributions and Shock Shape on an Oblate Spheroid at Mach Numbers of 3 and 6
The results of experimental measurements of the static pressure distribution and bow shock shape on an oblate sphereoid are presented. This experiment was conducted at nominal Mach numbers of 3 and 6 and a free stream Reynolds number range of 2.3 X 106 to 5.8 X 106 per foot. Comparisons are made with the calculated values of several different laboratories.