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FINITE-RATE INTERPHASE HEAT-TRANSFER EFFECTS ON MULTIPHASE BURNING IN CONFINED POROUS PROPELLANTS

机译:受限多孔推进剂中有限相间传热对多相燃烧的影响

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Deflagrations in porous solid propellants are often affected by an increasing pressure difference, or overpressure, between the burned-gas region and the gas deep within the pores of the material. As a result, there appears to be a relatively rapid change in the burning-rate response over a certain range of overpressures in which the sensitivity, or slope, of the propagation speed as a function of overpressure transitions from relatively small to large values. This is often referred to as a transition from "conductive" to "convective" burning, corresponding to the increased role played by convective gas transport relative to thermal diffusion in determining the propagation speed of the deflagration. In the present work, we consider the analysis of a two-temperature model in which finite-rate interphase heat-transfer effects also play an important role in determining the burning-rate eigenvalue. In particular, we revisit a physically relevant scenario in which the first effects of temperature nonequilibrium are felt in the thin multiphase reaction region, with the preheat zone remaining in thermal equilibrium to a first approximation. Expanding on previous asymptotic results that are further specialized to certain limiting parameter regimes, we consider a combination of analytical and numerical approaches to obtain solutions in the chemical boundary layer, and hence the burning-rate eigenvalue, for a significantly wider range of parameters. In particular, we are able to address a greater range of resistance to interphase heat transfer and thus determine an upper limit beyond which interphase temperature differences are no longer negligible in the preheat region. The main result is that, relative to earlier single-temperature models in which temperature-nonequilibrium effects are completely neglected, the burning-rate response exhibits a much sharper transition from the conduction- to the convection-dominated regime. This results from the ability of the reactive phase to retain a greater amount of the heat of reaction, causing a rapid increase in the reaction rate as the local temperature in that phase exceeds both the corresponding single-temperature value and even the final burned temperature.
机译:多孔固体推进剂的爆燃通常受燃烧气体区域与材料孔隙深处的气体之间压力差或超压增加的影响。结果,在一定范围的超压下,燃烧速率响应似乎出现了相对快速的变化,其中,传播速度的灵敏度或斜率根据超压从较小的值过渡到较大的值。这通常被称为从“传导”燃烧到“对流”燃烧的过渡,对应于对流气体传输相对于热扩散在确定爆燃传播速度中所起的增加作用。在目前的工作中,我们考虑对双温度模型进行分析,在该模型中,有限速率的相间传热效应在确定燃烧速率特征值中也起着重要作用。特别是,我们重新审视了一个物理相关的场景,在该场景中,在薄的多相反应区域中感受到了温度不平衡的第一效应,而预热区则保持了热平衡,直到第一近似值。在进一步扩展以前专门针对某些极限参数方案的渐近结果的基础上,我们考虑了分析方法和数值方法的组合,以在更广泛的参数范围内获得化学边界层中的溶液,从而获得燃烧速率特征值。特别是,我们能够解决更大范围的相间传热阻力,从而确定一个上限,超过该上限,在预热区域中相间温差不再可以忽略不计。主要结果是,相对于完全忽略了温度非平衡效应的早期单温度模型,燃烧速率响应显示出从传导到对流为主的状态更加陡峭的过渡。这是由于反应相保留大量反应热的能力所致,因为该相中的局部温度超过了相应的单一温度值,甚至是最终的燃烧温度,反应速率也迅速提高。

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