\(H_{2}\) injection and combustion in a Mach 5 air inlet through a viscous Mach interaction

DOI10.1016/j.euromechflu.2010.03.007zbMath1196.76080OpenAlexW1983493322MaRDI QIDQ1959949

Ghislain Tchuen, David E. Zeitoun, Yves Burtschell

Publication date: 12 October 2010

Published in: European Journal of Mechanics. B. Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.euromechflu.2010.03.007

zbMATH Keywords

VMIhypersoniccombustion processesDMI\(H_{2}\) injectionRIspace airplane

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Combustion (80A25) Reaction effects in flows (76V05) Hypersonic flows (76K05)

Uses Software

• Spalart-Allmaras

Cites Work

• Shock/shock and shock/boundary layer interactions in an axisymmetric steady laminar flow
• Numerical investigation of \(H_2\) injection in Mach 5 air flow with a strong shock/boundary layer interaction
• Density corrections for turbulence models

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