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O. M. Kolesnikov 《Combustion, Explosion, and Shock Waves》2006,42(1):41-47
A method and results of computing the influence of unmixedness in large eddies generated by instability of a contact discontinuity
on ignition and combustion of turbulent jets of a fuel in a supersonic flow are presented. The basic system of equations is
the Reynolds-averaged Navier-Stokes equations. The influence of unmixedness on chemical reaction rates is reproduced by using
a random number generator adjusted in accordance with the probability of origination of favorable conditions for proceeding
of chemical reactions, which is computed in each node of the computational grid. The problem of combustion of a plane hydrogen
jet injected into a supersonic flow along the plate surface is considered as an example. It is shown that allowance for unmixedness
in the case where the flow and the jet have favorable initial parameters for self-ignition leads to a delay in heat release
and to origination of pressure and temperature fluctuations. As the parameters approach the self-ignition limit, these fluctuations
increase, and the combustion becomes intermittent.
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Translated from Fizika Goreniya i Vzryva, Vol. 42, No. 1, pp. 49–56, January–February, 2006. 相似文献
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