Investigation of a hypersonic viscous shock layer on rotating axisymmetric bodies in the presence of blowing

DOI10.1007/BF01051107zbMath0602.76073MaRDI QIDQ1082203

B. George

Publication date: 1986

Published in: Fluid Dynamics (Search for Journal in Brave)

zbMATH Keywords

stagnation pointfinite-difference methodshock layerviscous compressible gasheat transfer coefficientsblunt axisymmetric bodieshypersonic flow of a laminar streamrotating axisymmetric bodiesshock wave separation

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Hypersonic flows (76K05) Basic methods in fluid mechanics (76M99)

Cites Work

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• Influence of rotation of the body and exterior vorticity on the heat transfer near the stagnation point of a blunt body in a supersonic stream
• Determination of the parameters of the boundary layer on rotating axisymmetric cones

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