Turbulence and additive effects on ignition delay in supersonic combustion
AM Tahsini - Proceedings of the Institution of Mechanical …, 2013 - journals.sagepub.com
Proceedings of the Institution of Mechanical Engineers, Part G …, 2013•journals.sagepub.com
Numerical study of two-dimensional supersonic hydrogen–air mixing layer is performed to
investigate the effects of turbulence and chemical additive on ignition distance. Chemical
reaction is treated using detail kinetics. Advection upstream splitting method is used to
calculate the fluxes, and one-equation turbulence model is chosen here to simulate the
considered problem. Hydrogen peroxide is used as an additive and the results show that
inflow turbulence and chemical additive may drastically decrease the ignition delay in …
investigate the effects of turbulence and chemical additive on ignition distance. Chemical
reaction is treated using detail kinetics. Advection upstream splitting method is used to
calculate the fluxes, and one-equation turbulence model is chosen here to simulate the
considered problem. Hydrogen peroxide is used as an additive and the results show that
inflow turbulence and chemical additive may drastically decrease the ignition delay in …
Numerical study of two-dimensional supersonic hydrogen–air mixing layer is performed to investigate the effects of turbulence and chemical additive on ignition distance. Chemical reaction is treated using detail kinetics. Advection upstream splitting method is used to calculate the fluxes, and one-equation turbulence model is chosen here to simulate the considered problem. Hydrogen peroxide is used as an additive and the results show that inflow turbulence and chemical additive may drastically decrease the ignition delay in supersonic combustion.
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