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Acoustic response of near-equilibrium diffusion flames with large activation energies

机译:具有大活化能的近平衡扩散火焰的声响应

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The interaction of nonpremixed flamelets with acoustic pressure waves of large characteristic wavelength, central to the development of acoustic instabilities in liquid-propellant rocket engines, is investigated by evaluating the periodic response of a counterflow diffusion flame subject to a harmonic pressure variation. An irreversible step with an Arrhenius rate having a large activation energy is used to model the exothermic reaction between the fuel and the oxidizer. The interactions of the chemistry with the prescribed time-dependent pressure variations are analyzed by numerical and asymptotic methods for large values of the Zel'dovich number β » 1 measuring the temperature dependence of the heat-release rate and small values of the relative amplitude ∈ « 1 of the pressure fluctuation, with the the product β∈ assumed to be of order unity in the distinguished limit addressed. Evaluations of the local Rayleigh index for β∈« 1 indicate that finite-rate chemical-kinetic effects dominate the acoustic pressure response of strained flamelets under conditions near diffusion-flame extinction. For robust, diffusion-controlled flames, on the other hand, unsteady modifications to the outer chemical-equilibrium transport regions flanking the reaction layer are more important but produce only moderate effects on acoustic instabilities.
机译:通过评估逆流扩散火焰在谐波压力变化下的周期性响应,研究了非预混小火焰与大特征波长声压波之间的相互作用,这是液体推进火箭发动机声不稳定性发展的关键。具有大活化能的阿累尼乌斯率的不可逆步骤用于模拟燃料和氧化剂之间的放热反应。通过数值和渐近方法分析了化学物质与规定的随时间变化的压力变化之间的相互作用,其中大的Zel'dovich数β»1可以测量放热率的温度依赖性,而小的相对幅度ε则较小。 «压力波动的1,乘积βε在所确定的极限中假定为阶次单位。对β∈«1的局部瑞利指数的评估表明,在接近扩散火焰熄灭的条件下,有限速率化学动力学效应主导着应变小焰的声压响应。另一方面,对于鲁棒的,受扩散控制的火焰,对反应层两侧的外部化学平衡传输区域进行不稳定的修改更为重要,但只会对声音的不稳定性产生中等程度的影响。

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