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Aerodynamic Force Measurements Over Missile Configuration in IISC Shock Tunnel At M-Infinity = 3.85 And 9.15

Raju, C and Reddy, NM (1990) Aerodynamic Force Measurements Over Missile Configuration in IISC Shock Tunnel At M-Infinity = 3.85 And 9.15. In: Experiments in Fluids, 10 (2-3). 175-177 .

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Official URL: http://www.springerlink.com/content/t4128002482307...
Item Type: Editorials/Short Communications
Additional Information: Copyright of this article belongs to Springer.
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)
Date Deposited: 06 Jan 2011 11:54
Last Modified: 06 Jan 2011 11:54
URI: http://eprints.iisc.ernet.in/id/eprint/34864

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