Ignition in the supersonic hydrogen/air mixing layer with reduced reaction mechanisms

DOI10.1017/S0022112096002790zbMath0888.76088OpenAlexW2052636119MaRDI QIDQ4350987

Hong G. Im, Chung K. Law, Su-Ryong Lee, Brian T. Helenbrook

Publication date: 4 September 1997

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

Full work available at URL: https://doi.org/10.1017/s0022112096002790

zbMATH Keywords

asymptotic analysisturning pointbranchingthermal runawaylow-temperature regimehigh-temperature regimecharacteristic temperature of reaction zone

Mathematics Subject Classification ID

Combustion (80A25) Reaction effects in flows (76V05) Supersonic flows (76J20)

Related Items (4)

A detailed verification procedure for compressible reactive multicomponent Navier-Stokes solvers ⋮ Diffusion flame in a two-dimensional, accelerating mixing layer ⋮ A theoretical study of spontaneous ignition of fuel jets in an oxidizing ambient with emphasis on hydrogen jets ⋮ Auto-ignition of a homogeneous hydrogen–air mixture subjected to unsteady temperature fluctuations

Cites Work

• Ignition and structure of a laminar diffusion flame in a compressible mixing layer with finite rate chemistry
• A note on the laminar mixing of two uniform parallel semi-infinite streams

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