To the problem of modeling gas flows behind the strong shock wave front using an effective adiabatic index

DOI10.1134/S1063454120010033zbMath1457.76093OpenAlexW3159113142MaRDI QIDQ2227816

V. I. Bogatko, Elena A. Potekhina

Publication date: 15 February 2021

Published in: Vestnik St. Petersburg University. Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1063454120010033

zbMATH Keywords

adiabatic index discontinuity

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Gas dynamics (general theory) (76N15)

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Cites Work

• An 'Ideal equivalent gas method' for the study of shock waves in supersonic real gas flows
• Radiative Transfer Effects on Reflected Shock Waves I. Transparent Gas
• The instability of liquid surfaces when accelerated in a direction perpendicular to their planes. I
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