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Experimental Investigation of Film Cooling Technique over a Blunt Body in Hypersonic Flow

  • J. L. K. Sindhu
  • S. Mohammed Ibrahim
  • K. P. J. Reddy
Conference paper

Abstract

As an alternative to conventional TPS (thermal protection system), film cooling technique has been previously extensively studied. The aim of the current work is to inject new coolants, i.e., mist (atomized water particles) and N2-CO2 mixture, and study the heat transfer variation over the surface of a blunt body in hypersonic flow.

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Copyright information

© Springer International Publishing AG, part of Springer Nature 2019

Authors and Affiliations

  • J. L. K. Sindhu
    • 1
  • S. Mohammed Ibrahim
    • 1
  • K. P. J. Reddy
    • 1
  1. 1.Laboratory for Hypersonics and Shock Wave Research, Department of Aerospace EngineeringIndian Institute of ScienceBangaloreIndia

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