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- W157466771 abstract "An experimental investigation was conducted in the GALCIThypersonic blow-down tunnel to determine surface pressure distributions and shock wave shapes for a series of sharp-nosed and slightly-blunted bodies of revolution at a nominal Mach number of 18.4 and a free stream Reynolds number of 6.20 x 10^5 per inch. The four bodiesinvestigated were as follows: (1) 15° half-angle sharp cone; (2) 15° half-angle spherically-blunt cone (bluntness ratio= .24); (3) 20° half-angle sharp cone; (4) 2/3-power body.The pressure distributions on the sharp cones agreed wellwith the Taylor-Maccoll theory. As expected, the pressure near the nose of the blunt cone was much higher than predicted by this theory, but the pressure decreases monotonically to a value lower than thetheoretical value on the conical skirt, indicating that the flow has over-expanded. The measured shock wave shape for the 2/3-power body was found to be proportional to x^(0.69), and the shock wave ordinates agree closely with those predicted by Cole and by Kubota and Lees. Measured surface pressure distributions on the 2/3-powerbody are predicted satisfactorily by the Kubota-Lees analysis. A simple correction for boundary layer growth accounts for most of the increase in pressure on the rear portion of the body over the values predicted by inviscid theory." @default.
- W157466771 created "2016-06-24" @default.
- W157466771 creator A5084847071 @default.
- W157466771 date "1956-12-15" @default.
- W157466771 modified "2023-09-23" @default.
- W157466771 title "A Preliminary Experimental Investigation of the Flow over Simple Bodies of Revolution at M=18.4 in Helium" @default.
- W157466771 doi "https://doi.org/10.7907/x3hz-bn39." @default.
- W157466771 hasPublicationYear "1956" @default.
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