Numerical and theoretical study of the shock stand-off distance in non-equilibrium flows

DOI10.1017/S0022112008001973zbMath1146.76029OpenAlexW2074911473MaRDI QIDQ3530767

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Publication date: 20 October 2008

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/s0022112008001973

zbMATH Keywords

kinetic approachvibrational energychemical relaxationgeneralized Chapman-Enskog method

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20) Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05) Reaction effects in flows (76V05) Hypersonic flows (76K05)

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Computational Study of Hypersonic Rarefied Gas Flow over Re-Entry Vehicles Using the Second-Order Boltzmann-Curtiss Constitutive Model ⋮ Physical criterion study on forward stagnation point heat flux CFD computations at hypersonic speeds ⋮ Extension of CE/SE method to non-equilibrium dissociating flows ⋮ Shock layers over blunt and conical bodies in hypersonic non-equilibrium flow ⋮ Hypersonic flow over spherically blunted cone capsules for atmospheric entry. Part 2. Vibrational non-equilibrium effects

Cites Work

• The solution of the Navier-Stokes equations using Gauss-Seidel line relaxation
• Inviscid flow of a reacting mixture of gases around a blunt body
• A theoretical model for the shock stand-off distance in frozen and equilibrium flows
• Non-equilibrium dissociating flow over spheres
• Non-equilibrium dissociating nitrogen flow over spheres and circular cylinders

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