首页> 外文会议>Israel annual conference on aerospace sciences >SPHERICAL FLAME FRONT PROPAGATION THROUGH A LIQUID FUEL MIST: FINITE RATE EVAPORATION AND DROPLET DRAG EFFECTS
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SPHERICAL FLAME FRONT PROPAGATION THROUGH A LIQUID FUEL MIST: FINITE RATE EVAPORATION AND DROPLET DRAG EFFECTS

机译:通过液体燃料雾的球形火焰前沿:有限速率蒸发和液滴拖动效应

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An evolution equation for a laminar flame front propagating into an air and liquid fuel mist cloud is derived for the first time, accounting for both finite rate evaporation of the fuel droplets and the slip velocity between them and their host environment. The asymptotic analysis employed for developing the equation exploits the usual inverse large activation energy parameter associated with chemical reaction in the flame and a small drag parameter. It is demonstrated that, in the no slip velocity case, increasing the vaporization Damkohler number can produce flame extinction presumably due to the more intense heat loss incurred due to droplet heat absorption for vaporization. Droplet drag can also induce extinction due to the longer residence time of the droplets in any locale leading to more vaporization with a greater attendant heat loss. The predicted results for droplet velocity are compared to independent experimental data from the literature with good qualitative agreement.
机译:首次推导到空气和液体燃料雾云中传播到空气和液体燃料雾云中的流动式的演化方程,占燃料液滴的有限速率蒸发和它们之间的滑动速度及其宿主环境。用于开发等式所采用的渐性分析利用了与火焰中的化学反应相关的通常的逆大激活能量参数和小型阻力参数。据证明,在没有滑动速度壳体中,增加蒸发达摩洛克勒数可以产生火焰灭绝,这可能是由于由于液滴吸热而导致的蒸发而产生的热量损失更强烈。由于任何区域设置的液滴中的延长时间较长,液滴阻力也可以引起灭绝,导致具有更高的伴随的热量损失的蒸发。将液滴速度的预测结果与来自文献的独立实验数据进行比较,具有良好的定性协议。

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