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Computational Investigations of Impingement Heat Transfer on an Effused Concave Surface

  • Kumar, M. Ashok (Thermal Turbomachines Laboratory, Department of Mechanical Engineering, Indian Institute of Technology Madras) ;
  • Prasad, Bhamidi V.S.S.S. (Thermal Turbomachines Laboratory, Department of Mechanical Engineering, Indian Institute of Technology Madras)
  • Received : 2012.05.08
  • Accepted : 2012.04.17
  • Published : 2012.06.30

Abstract

A computational study is reported on flow and heat transfer characteristics from five rows of circular air jets impinging on a concave surface with four rows of effusion holes. The effects of exit configurations of spent air and the arrangement of jet orifices and effusion holes for a jet Reynolds number of 7500 is investigated. In all, eight cases are studied and a good qualitative correlation is found among their flow patterns, pressure variations and heat transfer distributions.

Keywords

References

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