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

DOI10.1007/BF01093921zbMath0556.76051MaRDI QIDQ761144

D. Kharzeev

Publication date: 1984

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

zbMATH Keywords

iterative numerical methodaxisymmetric cooled surfacehypersonic viscous shock layerlongitudinal vorticityrotation about longitudinal axisthin three-dimensional shock layer

Mathematics Subject Classification ID

Hypersonic flows (76K05)

Related Items (5)

Investigation of a hypersonic viscous shock layer on rotating axisymmetric bodies in the presence of blowing ⋮ Viscous shock layer near the stagnation point on a rotating body with unsteady injection and surface cooling ⋮ Hypersonic viscous shock layer in a swirling gas flow on a permeable surface ⋮ Supersonic swirling flow past a blunt body ⋮ Mathematical simulation of nonequilibrium shock layer flow around a rotating body

Cites Work

• Flow regimes of a viscous gas in a thin three-dimensional shock layer near a surface with small curvatures
• Investigation of stationary flow of viscous gas in a thin three- dimensional shock layer

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