Aerodynamic drag reduction by heat addition into the shock layer for a large angle blunt cone in hypersonic flow

DOI10.1063/1.2944982zbMath1182.76411OpenAlexW2031639135MaRDI QIDQ5304080

K. P. J. Reddy, G. M. Hegde, Gopalan Jagadeesh, E. Arunan, Vinayak Kulkarni

Publication date: 18 March 2010

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

Full work available at URL: https://semanticscholar.org/paper/3eb8de2a4bf9683fe7af4e462247788eb68ba1d4

zbMATH Keywords

shock wavesdrag reductionhypersonic flowenthalpychromiumoxygenflow visualisationthermochemistrychemically reactive flow

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Cites Work

• Counterflow drag reduction by supersonic jet for a blunt body in hypersonic flow
• Effect of concentrated energy deposition on the aerodynamic drag of a blunt body in hypersonic flow

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