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Shock tunnel testing of a Mach 6 hypersonic waverider

Hemanth, K and Jagadeesh, G and Saravanan, S and Nagashetty, K and Reddy, KPJ (2009) Shock tunnel testing of a Mach 6 hypersonic waverider. In: 26th International Symposium on Shock Waves, JUL 15-20, 2007, Gottingen, Germany, pp. 701-706.

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Official URL: http://www.springerlink.com/content/w04h0hp5g7lu67...

Abstract

A waverider is a lifting body configuration whose upper surface is parallel to the free stream, and the lower surface aerodynamically so designed, that the resulting shock at the design Mach number, is always attached with the leading edge of the vehicle. This prevents spillage from high pressure (lower) surface to the low pressure (upper) surface.In the present study a conical waverider has been designed, fabricated and tested at Mach 6 in the IISc hypersonic shock tunnel HST2. The measurements show that the waverider has a lift to drag ratio of 4.28 at the designed Mach number. Exhaustive FEM and CFD studies are also carried out to complement the force measurements in the tunnel.

Item Type: Conference Paper
Additional Information: Copyright of this article belongs to Springer.
Department/Centre: Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)
Date Deposited: 16 Dec 2009 09:28
Last Modified: 16 Dec 2009 09:28
URI: http://eprints.iisc.ernet.in/id/eprint/23673

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