Effect of physical and chemical nonequilibrium processes on the parameters of the near wake downstream of a spacecraft

DOI10.1134/S0015462809050172zbMath1215.76114OpenAlexW1980385992MaRDI QIDQ545716

A. B. Gorshkov

Publication date: 22 June 2011

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

Full work available at URL: https://doi.org/10.1134/s0015462809050172

zbMATH Keywords

Navier-Stokes equationsnear wakehypersonic flowblunt conenonequilibrium air

Mathematics Subject Classification ID

Reaction effects in flows (76V05) Hypersonic flows (76K05)

Cites Work

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• Slip boundary conditions on a catalytic surface in a multicomponent gas flow
• Comparison of the calculated results for hypersonic flow past blunt bodies with the OREX flight test data
• Laminar base flow downstream of slender cones in hypersonic flow
• Artificial dissipation models for the Euler equations
• Reacting Shock Layers with Slip and Catalytic Boundary Conditions
• Nonequilibrium Effects in Near-Wake Ionizing Flows
• Chemical Relaxation with Preferential Dissociation from Excited Vibrational Levels

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