Mathematical model of detonation combustion of kerosene vapor in an oxidizer

Springer Science and Business Media LLC - Tập 48 - Trang 41-48 - 2012
A. V. Fedorov1, D. A. Tropin1
1Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences, Novosibirsk, Russia

Tóm tắt

A mathematical model is proposed to describe ignition and combustion of a hydrocarbon fuel (kerosene vapor in air). Based on an analysis of experimental data on the ignition delay dependence on temperature, approximation formulas are derived for the ignition delay as a function of species concentrations and of the pressure and temperature of the mixture. A method for determining the pre-exponent in the kerosene combustion kinetic equation as a function of the local temperature of the mixture is proposed, which provides a reasonably accurate description of the time of mixture combustion. Based on this kinetics, the structure of the detonation wave in a stoichiometric kerosene-air mixture and in a mixture with a reduced fraction of the oxidizer for the Chapman-Jouguet and overdriven detonation regimes is described.

Tài liệu tham khảo

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