作者: B. Deshaies , L. F. Figueira Da Silva , M. René-Corail
DOI: 10.1007/978-94-011-5432-1_2
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摘要: A comprehensive analysis of the mechanisms and parameters which control self-ignition stabilization Hydrogen-Air combustion in supersonic shear layers is presented. This based on extensive numerical results obtained for unpremixed premixed basic flow configurations, namely mixing co-flowing jets, boundary oblique shock waves.