The applicability of continuum models in the transitional regime of hypersonic flow over blunt bodies

DOI10.1016/J.JAPPMATHMECH.2009.11.003zbMath1272.76160OpenAlexW2048385577MaRDI QIDQ370399

I. G. Brykina, G. A. Tirskij, Boris V. Rogov

Publication date: 19 September 2013

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: http://www.sciencedirect.com/science/article/pii/S0021892809001385

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05) Hypersonic flows (76K05)

Related Items (5)

Generalized viscous shock layer equations with slip conditions on a surface in a flow field and on a head shock ⋮ Asymptotic solutions of the thin viscous shock layer equations near the symmetry plane of blunt bodies in hypersonic rarefied gas flow ⋮ The effect of surface curvature on the boundary conditions in the viscous shock layer model for hypersonic rarefied gas flow ⋮ A comparative analysis of approaches for investigating hypersonic flow over blunt bodies in a transitional regime ⋮ Asymptotic investigation of heat transfer and skin friction in three-dimensional hypersonic rarefied gas flows

Cites Work

• Asymptotic solution of the two-dimensional equations for a thin viscous rarefied shock layer on a cold surface
• Asymptotic solutions of the two-dimensional equations for a thin viscous shock layer in a rarefied gas
• Hyperbolic approximation of the Navier-Stokes equations for viscous mixed flows
• Numerical solution of the hypersonic viscous shock-layer equations
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