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Droplet combustion experiments in varying forced convection using microgravity environment

机译:微重力环境下不同强制对流的液滴燃烧实验

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A new microscopic model of the interaction between droplet flames and fine vortex tubes which compose a coherent structure of turbulence was developed. Three non-dimensional numbers were introduced to extend the length scale and time scale so as to be suitable for microgravity experiments using droplets of combustion of about 1 mm in diameter. An experimental apparatus for combustion of a single droplet and that of an array of two droplets in varying airflow was developed, and experiments were performed in microgravity and normal gravity at pressures up to 2.0 MPa for n-nonane and ethanol as fuels. Variations of the instantaneous burning rate constant, K_i, in response to the varying flow velocity was successfully observed. At high pressure, the effects of droplet Reynolds number Re on K_i was clearly seen, while the effects of natural convection, which increases K_i with Re, was seen in normal gravity even in the forced airflows. As for the experiments on combustion of an array of two droplets, K_i reduction of the downstream droplet became weak when the flow direction was varied. However, the K_i reduction of the downstream droplet for flow direction variations was clearly seen for n-nonane droplets but almost not for ethanol droplets. The interaction mechanism between upstream and downstream droplets is considered to result from the elimination of oxidizer supply to the downstream droplet, indicating strong interaction effects of n-nonane droplets for a stoichiometric oxygen-fuel ratio of n-nonane (i.e., 14.0) greater than that of ethanol (i.e., 3.0).
机译:建立了液滴火焰与细小涡管之间相互作用的新微观模型,该模型构成了湍流的连贯结构。引入了三个无量纲数字以扩展长度尺度和时间尺度,以适合使用直径约1 mm的燃烧液滴进行微重力实验。开发了用于在变化的气流中燃烧单个液滴和两个液滴的阵列的燃烧的实验设备,并且以正壬烷和乙醇为燃料,在微重力和法向重力下以高达2.0 MPa的压力进行了实验。成功观察到瞬时燃烧速率常数K_i随变化的流速而变化。在高压下,可以清楚地看到液滴雷诺数Re对K_i的影响,而在自然重力下,即使在强制气流中,也可以看到自然对流的影响(随Re增加K_i)。至于两个小滴的阵列燃烧的实验,当改变流动方向时,下游小滴的K_i还原变弱。但是,对于正壬烷液滴,可以清楚地看到下游液滴因流动方向变化而发生的K_i降低,而对于乙醇液滴则几乎看不到。上游和下游液滴之间的相互作用机理被认为是由于消除了向下游液滴的氧化剂供应,表明当正壬烷的化学计量氧-燃料比(即14.0)大于时,正壬烷液滴的强烈相互作用效应。乙醇(3.0)。

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