Кинетический вязкий ударный слой вблизи передней кромки тонкого вращающегося диска;Kinetyc viscous shock layer near leading edge of a thin rotating disc

DOI10.20948/mm-2023-11-07OpenAlexW4388140445MaRDI QIDQ6143328

A. L. Ankudinov

Publication date: 23 January 2024

Published in: Математическое моделирование (Search for Journal in Brave)

Full work available at URL: http://mathnet.ru/eng/mm4507

zbMATH Keywords

analytical solutionangle of attackkinetic pressurehypersonic nonequilibrium molecular gas flowNavier-Stokes analogy

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05) General theory of rotating fluids (76U05) Hypersonic flows (76K05)

Cites Work

• Unnamed Item
• Asymptotic solutions of the thin viscous shock layer equations near the symmetry plane of blunt bodies in hypersonic rarefied gas flow
• Rheology of rarefied gas flow in hypersonic shock and boundary layers
• The effect of surface curvature on the boundary conditions in the viscous shock layer model for hypersonic rarefied gas flow
• Approximate analytical solutions for heat fluxes in three-dimensional hypersonic flow over blunt bodies
• Asymptotic investigation of heat transfer and skin friction in three-dimensional hypersonic rarefied gas flows
• A comparative analysis of approaches for investigating hypersonic flow over blunt bodies in a transitional regime

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