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Measurement of aerodynamic forces and moments for missile shaped bodies in hypersonic shock tunnel using 6-component accelerometer based balance system

Saravanan, S and Jagadeesh, G and Reddy, KPJ (2007) Measurement of aerodynamic forces and moments for missile shaped bodies in hypersonic shock tunnel using 6-component accelerometer based balance system. In: 26th International Symposium on Shock Waves, Gottingen, Germany, 2007, Gottingen.

Full text not available from this repository.
Item Type: Conference Paper
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)
Date Deposited: 21 Oct 2011 10:22
Last Modified: 21 Oct 2011 10:22
URI: http://eprints.iisc.ernet.in/id/eprint/41592

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