Shock layers over blunt and conical bodies in hypersonic non-equilibrium flow

DOI10.1007/s00193-010-0264-0zbMath1267.76043OpenAlexW2054576896MaRDI QIDQ633508

Juan-Miguel Gracia

Publication date: 1 April 2011

Published in: Shock Waves (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00193-010-0264-0

zbMATH Keywords

hypersonic flownon-equilibrium gas dynamicsshock shapedensity flow-fieldvibrational-chemical coupling

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Supersonic flows (76J20)

Cites Work

• Unnamed Item
• The solution of the Navier-Stokes equations using Gauss-Seidel line relaxation
• Numerical and theoretical study of the shock stand-off distance in non-equilibrium flows
• Introduction to Reactive Gas Dynamics
• 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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