Mathematical simulation of nonequilibrium shock layer flow around a rotating body

DOI10.1134/S096554252201002XOpenAlexW4213071813MaRDI QIDQ2116208

A. L. Ankudinov

Publication date: 16 March 2022

Published in: Computational Mathematics and Mathematical Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s096554252201002x

zbMATH Keywords

hypersonic two-dimensional flowkinetic thin viscous shock layernonequilibrium with respect to internal and translational degrees of freedomnonthin axisymmetric blunt bodyrotation of body about axissingle-species polyatomic gas

Mathematics Subject Classification ID

Fluid mechanics (76-XX) Partial differential equations (35-XX)

Cites Work

• Unnamed Item
• Rheology of rarefied gas flow in hypersonic shock and boundary layers
• 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

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