A kinetic shock layer in the spreading plane of a lifting-body apparatus

DOI10.1134/S0015462821070028zbMath1491.76042OpenAlexW4200174661MaRDI QIDQ2668104

A. L. Ankudinov

Publication date: 3 March 2022

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0015462821070028

zbMATH Keywords

Navier-Stokes equationsnumerical solutionmacrokinetic thin viscous shock layernonequilibrium molecular gas

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05) Basic methods in fluid mechanics (76M99) Compressible Navier-Stokes equations (76N06)

Related Items (1)

On a paradoxical property of solving the problem of stationary flow around a body by a subsonic stratified flow of an ideal gas;Об одном парадоксальном свойстве решения задачи стационарного обтекания тела дозвуковым стратифицированным потоком идеального газа

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
• Perspective on hypersonic nonequilibrium flow

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