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A. K. Sreekanth

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Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnel

by A. K. Sreekanth First published in 1956 — 2 editions

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Aerodynamic predictive methods and their validation in hypersonic flows

by A. K. Sreekanth First published in 2003 — 1 edition

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Drag measurements of circular cylinders and spheres in the transition regime at a Mach number of 2

by A. K. Sreekanth First published in 1961 — 1 edition

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Drag measurements on circular cylinders and spheres in the transition regime at a Mach number of 2

by A. K. Sreekanth First published in 1961 — 1 edition

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OLID: OL1526408A

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Created April 1, 2008
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September 3, 2008	Edited by RenameBot	fix author name
April 1, 2008	Created by an anonymous user	initial import