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Stability of underexpanded supersonic jet flames burning H-2-CO mixtures

机译:膨胀不足的超音速喷射火焰燃烧H-2-CO混合物的稳定性

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摘要

It has been established experimentally that both natural gas and hydrogen discharges, through circular orifices larger than a critical diameter, sustain stable lifted flames irrespective of the reservoir pressure driving the release. At smaller diameters, however, stable burning will only be achieved at operating pressures higher than a particular, diameter-dependent, threshold. This latter is strongly fuel-type dependent but empirical correlations have been developed to describe such behaviour. Given the wide disparity of critical diameters depending upon the fuel type considered, the behaviour of multi-component gaseous mixtures involving hydrogen is much less predictable than the correlations for pure fuels might indicate. A series of experiments has been undertaken in which H-2-CO mixtures are discharged from a high pressure reservoir to ambient through convergent circular nozzles, varying in diameter from 1.3 to 5 mm. A wide range of driving pressures has been investigated, from 3 to 50 bar, embracing fuel mixtures containing up to 20% CO by volume. Stability curves have been derived that identify the region where stable burning is sustained relative to the pressure ratio (reservoir pressure/ambient pressure) and the CO concentration in the fuel mixture. The present experimental data are compared with existing correlations (Kalghatgi 1981), derived from subsonic releases, and Birch et al. (1988a), applied to underexpanded supersonic methane jet flames. Although these correlations reproduce the general trend observed experimentally, they appear to significantly over-estimate the stability region. Furthermore, they do not account for the high sensitivity of the diluent concentration on the blowout stability. A thorough investigation is carried out in order to determine the source of discrepancies observed between the empirical correlations and the present measurements. Differential diffusion between the fuel components is shown to be negligible. The introduction of additional information on the turbulent flowfield from numerical simulation of the isothermal underexpanded jet, immediately upstream of the flame stabilisation region, does not appear to yield discriminating evidence for incipient blow-off instability. The maximum burning velocity alone, a widely employed characterising parameter, does not appear to describe accurately the complex interactions between the turbulent flowfield and the chemical kinetics. [References: 27]
机译:通过实验已经确定,天然气和氢气都通过大于临界直径的圆形孔口排放,从而维持稳定的升起火焰,而与驱动释放的储层压力无关。但是,在较小的直径下,只有在高于特定于直径的特定阈值的工作压力下才能实现稳定燃烧。后者强烈依赖于燃料类型,但是已经建立了经验相关性来描述这种行为。考虑到临界直径的差异很大,取决于所考虑的燃料类型,涉及氢的多组分气态混合物的行为比纯燃料的相关性难以预测。已经进行了一系列实验,其中H-2-CO混合物通过直径从1.3到5毫米变化的会聚圆形喷嘴从高压储罐排放到环境中。已经研究了从3至50 bar的各种驱动压力,涵盖了按体积计最多含20%CO的燃料混合物。已经得出了稳定性曲线,该曲线确定了相对于压力比(储层压力/环境压力)和燃料混合物中CO浓度持续稳定燃烧的区域。目前的实验数据与现有的相关性(Kalghatgi 1981)进行了比较,这些相关性来自亚音速释放,Birch等。 (1988a),适用于超音速甲烷喷流火焰。尽管这些关联重现了实验观察到的总体趋势,但它们似乎大大高估了稳定区域。此外,它们没有考虑稀释剂浓度对井喷稳定性的高度敏感性。为了确定经验相关性与当前度量之间观察到的差异的来源,进行了彻底的调查。燃料组分之间的差异扩散显示为可忽略的。通过等温欠膨胀射流的数值模拟(紧接在火焰稳定区域的上游),在湍流场中引入附加信息,似乎并不能提供关于初发吹气不稳定的判别证据。仅最大燃烧速度,即广泛使用的表征参数,似乎无法准确地描述湍流场与化学动力学之间的复杂相互作用。 [参考:27]

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