On mathematical modeling of a hypersonic flow past a thin wing with variable shape

DOI10.1134/S1063454121040038zbMath1484.76036OpenAlexW4285355520MaRDI QIDQ2668901

V. I. Bogatko, Elena A. Potekhina

Publication date: 9 March 2022

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

Full work available at URL: https://doi.org/10.1134/s1063454121040038

zbMATH Keywords

asymptotic solutionsmall parameterintegro-differential equationEuler-Ampère transformsemi-inverse method: thin shock-layer method

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Asymptotic methods, singular perturbations applied to problems in fluid mechanics (76M45) Hypersonic flows (76K05)

Cites Work

• Hypersonic flow of gas over a slender wing of variable shape
• To the problem of modeling gas flows behind the strong shock wave front using an effective adiabatic index
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