Counterflow drag reduction by supersonic jet for a blunt body in hypersonic flow

DOI10.1063/1.2401623zbMath1146.76559OpenAlexW2029343207MaRDI QIDQ3531744

K. P. J. Reddy, Gopalan Jagadeesh, Balla Venukumar

Publication date: 3 November 2008

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

Full work available at URL: https://doi.org/10.1063/1.2401623

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Related Items (3)

Enhancement in counterflow drag reduction by supersonic jet in high enthalpy flows ⋮ Aerodynamic drag reduction by heat addition into the shock layer for a large angle blunt cone in hypersonic flow ⋮ Experimental investigation of drag reduction by forward facing high speed gas jet for a large angle blunt cone at Mach 8

Cites Work

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

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