Asymptotic model of a thin shock layer near a wedge/cone for the Burnett approximation

DOI10.1134/S2070048211020013zbMath1224.76086OpenAlexW2039873209MaRDI QIDQ3082255

A. L. Ankudinov

Publication date: 9 March 2011

Published in: Mathematical Models and Computer Simulations (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s2070048211020013

zbMATH Keywords

hypersonic flowsshock waves and blast waves

Mathematics Subject Classification ID

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

Related Items (1)

Asymptotic Burnett model of the gas flow in a thin shock layer near a cylinder

Cites Work

• Stabilization of the Burnett equations and application to hypersonicflows
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