Shock Waves pp 701-706

Shock tunnel testing of a Mach 6 hypersonic waverider

  • K. Hemanth
  • G. Jagadeesh
  • S. Saravanan
  • K. Nagashetty
  • K.P.J. Reddy
Conference paper

DOI: 10.1007/978-3-540-85168-4_113

Cite this paper as:
Hemanth K., Jagadeesh G., Saravanan S., Nagashetty K., Reddy K. (2009) Shock tunnel testing of a Mach 6 hypersonic waverider. In: Hannemann K., Seiler F. (eds) Shock Waves. Springer, Berlin, Heidelberg

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.

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Copyright information

© Springer-Verlag Berlin Heidelberg 2009

Authors and Affiliations

  • K. Hemanth
    • 1
  • G. Jagadeesh
    • 1
  • S. Saravanan
    • 1
  • K. Nagashetty
    • 1
  • K.P.J. Reddy
    • 1
  1. 1.Department of Aerospace EngineeringIndian Institute of ScienceIndia

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