Film cooling effectiveness on a large angle blunt cone flying at hypersonic speed

DOI10.1063/1.1862261zbMath1187.76457OpenAlexW1993268748MaRDI QIDQ3554942

S. Saravanan, Gopalan Jagadeesh, Niranjan Sahoo, K. P. J. Reddy, Vinayak Kulkarni

Publication date: 22 April 2010

Published in: Physics of Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1063/1.1862261

zbMATH Keywords

convectionMach numberhypersonic flowcoolingdragstagnation flowaerodynamicsenthalpyexternal flowsfilmscoolants

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Related Items (4)

Enhancement in counterflow drag reduction by supersonic jet in high enthalpy flows ⋮ Counterflow drag reduction by supersonic jet for a blunt body in hypersonic flow ⋮ Experimental investigation of drag reduction by forward facing high speed gas jet for a large angle blunt cone at Mach 8 ⋮ Heat transfer -- a review of 2005 literature

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