Hypersonic viscous shock layer in a swirling gas flow on a permeable surface

DOI10.1007/BF02628020zbMath0626.76072MaRDI QIDQ581145

S. V. Peĭgin, È. A. Gershbeĭn

Publication date: 1986

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

zbMATH Keywords

first approximationmethod of successive approximationsviscous shock layerviscous compressible gasparabolized Navier-Stokes equationsfree- stream flowhypersonic swirling flowrotating axisymmetric bluntweak injection

Mathematics Subject Classification ID

Flows in porous media; filtration; seepage (76S05) Transonic flows (76H05) Gas dynamics (general theory) (76N15) General theory of rotating fluids (76U05) 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
• A three-dimensional hypersonic viscous shock layer in two-phase flow
• Numerical simulation of steady supersonic flow over spinning bodies of revolution
• Integration of hypersonic viscous shock layer equations by a successive approximation method

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