Shock Waves pp 577-582

Effect of electric arc discharge on hypersonic blunt body drag

  • K. Satheesh
  • G. Jagadeesh
Conference paper

DOI: 10.1007/978-3-540-85168-4_92

Cite this paper as:
Satheesh K., Jagadeesh G. (2009) Effect of electric arc discharge on hypersonic blunt body drag. In: Hannemann K., Seiler F. (eds) Shock Waves. Springer, Berlin, Heidelberg

Summary

Experimental results on the effect of energy deposition using an electric arc discharge, upstream of a 60° half angle blunt cone configuration in a hypersonic flow is reported.Investigations involving drag measurements and high speed schlieren flow visualization have been carried out in hypersonic shock tunnel using air and argon as the test gases; and an unsteady drag reduction of about 50% (maximum reduction) has been observed in the energy deposition experiments done in argon environment. These studies also show that the effect of discharge on the flow field is more pronounced in argon environment as compared to air, which confirms that thermal effects are mainly responsible for flow alteration in presence of the discharge.

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Copyright information

© Springer-Verlag Berlin Heidelberg 2009

Authors and Affiliations

  • K. Satheesh
    • 1
  • G. Jagadeesh
    • 1
  1. 1.Dept. of Aerospace EngineeringIndian Institute of ScienceIndia

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