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Some Exploratory Tests on a Two-Dimensional Blown-Cylinder Model in the R.A.E. 2ft x I1/2ft Transonic Wind Tunnel

机译:R.a.E.中二维吹气缸模型的探索性试验2英尺x1 / 2英尺跨音速风洞

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摘要

Statio pressure measurements have been made at subsonic Mach numbers to examine compressibility effects on a two-dimensional circular cylinder with two tangential blowing slots. These results together with forces derived from them are briefly discussed.

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