Numerical investigation of \(H_2\) injection in Mach 5 air flow with a strong shock/boundary layer interaction

DOI10.1007/S00193-004-0230-9zbMath1136.76382OpenAlexW2071391583MaRDI QIDQ1769883

Yves Burtschell, David E. Zeitoun

Publication date: 30 March 2005

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

Full work available at URL: https://doi.org/10.1007/s00193-004-0230-9

zbMATH Keywords

finite volume methodcombustioninjectionshock/boundary-layer interactionsshock/shock interactions

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Finite volume methods applied to problems in fluid mechanics (76M12) Combustion (80A25) Viscous-inviscid interaction for compressible fluids and gas dynamics (76N17)

Related Items (1)

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

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