The measured static-pressure distributions at the model surfaces and in the surrounding flow field are presented for a related series of bodies of revolution having locations of maximum cross-sectional areas at 0.3, 0.4, 0.5, 0.6, and 0.7 of the body length. The data were obtained with the various bodies, all of fineness ratio 12, at zero angle of attack. The Mach number varied from 0.80 to 1.20, and the Reynolds number (based on body length) varied from approximately 23.4xl06 to 24.6xl06.
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