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- W2167067898 abstract "Wind tunnel tests were made for spheres of various sizes over a range of Mach numbers and Reynolds numbers. The results indicated some conditions where the drag was affected by changes in the afterbody pressure due to a shock reflection from the tunnel wall. This effect disappeared when the Mach number was increased for a given sphere size or when the sphere size was decreased for a given Mach number. Drag measurements and Schlieren photographs show the possibility of obtaining inaccurate data when tests are made with a sphere too large for the test section size and Mach number. Tests were also made of an oblate spheroid. The results indicated a region at high Mach numbers where inherent positive static stability might occur with the oblate-face forward. The drag results are compared with those for a sphere and those for various other shapes. The drag results for the oblate spheriod and the sphere are also compared with some calculated results." @default.
- W2167067898 created "2016-06-24" @default.
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- W2167067898 date "1991-04-09" @default.
- W2167067898 modified "2023-09-27" @default.
- W2167067898 title "Aerodynamics of spheres for Mach numbers from 0.6 to 10.5 including some effects of test conditions" @default.
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- W2167067898 doi "https://doi.org/10.2514/6.1991-894" @default.
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