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Burn Angle and Its Implications on Flame Spread Rate, Mass Burning Rate, and Fuel Temperature for Downward Flame Spread over Thin PMMA

机译:烧伤角度及其对火焰扩散速率,大规模燃烧速率和向下火焰燃料温度的影响,在薄的PMMA上传播

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摘要

ABSTRACT A burn angle is defined as the acute angle subtended by the pyrolyzing surface with the virgin fuel surface and is an easily measurable overall characteristic parameter of flame spread, just like flame height and spread rate. Downward flame spread and space-based microgravity experiments are conducted using polymethyl-methacrylate (PMMA) samples with thickness between 50 μm and 3 mm to correlate the burn angle with mass burning rate, an average temperature of the pyrolysis region, and flame spread rate. For very thin fuels, the burn angle is deduced from the ratio of fuel thickness and length of the pyrolysis region, whereas for relatively thicker fuels it is directly measured. Direct and indirect measurements of burn angles, as well as data from literature, show an initial increase of their values with fuel thickness, and after reaching a peak they decrease asymptotically in the limit of semi-infinite fuel beds. A simplified phenomenological model is developed to describe the burn angle behavior as a function of fuel thickness and is used to successfully predict the average burning rate and the length of the pyrolysis zone. The peak reached by the burn angle after the initial rise can only be explained if the average temperature of the pyrolysis region is assumed to vary with fuel thickness; the thinner the fuel, the higher the temperature. Although direct experiments are needed to verify this prediction, numerical solutions obtained with an existing code corroborate this conclusion.
机译:摘要将燃烧角定义为与原始燃料表面的热解表面赋予的锐角,并且是一种易于可测量的火焰涂抹的总体特征参数,就像火焰高度和扩散速率一样。使用厚度在50μm和3mm之间的聚甲基 - 甲基丙烯酸甲酯(PMMA)样品进行向下火焰扩散和空间的微刻度实验,以将燃烧角与质量燃烧速率,热解区域的平均温度和火焰扩散速率相关。对于非常薄的燃料,从热解区域的燃料厚度和长度的比率推导出燃烧角,而对于相对较厚的燃料,它是直接测量的。燃烧角的直接和间接测量,以及文献中的数据,显示它们的燃料厚度的初始增加,并且在达到半无限燃料床的极限中渐近的峰值后达到峰值。开发了一种简化的现象模型,以描述作为燃料厚度的函数的燃烧角度行为,用于成功预测热解区域的平均燃烧速率和长度。只有在初始上升后达到燃烧角达到的峰值只有在假定热解区域的平均温度以燃料厚度变化时才可以解释;燃料较薄,温度越高。虽然需要直接实验来验证这种预测,但是通过现有代码获得的数值解决方案证实了这一结论。

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