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Turbulence effects on evaporation rate-controlled spray combustor performance

机译:湍流对蒸发速率控制的喷雾燃烧器性能的影响

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We consider here the effects of gas-phase turbulence on the evaporation dynamics of a polydispersed dilute fuel spray in an adiabatic well-stirred reactor (WSR) supplied with hot compressed air. Turbulence increases the time-averaged rate of heat diffusion-controlled droplet evaporation but the augmentation factor is droplet size-dependent because of droplet inertia and evaporative drag reduction. Consequently, each droplet in a spray population will not be characterized by the same rate of area change even in the same time-averaged environment. When these physical phenomena are convoluted with the residence time distribution characterizing a WSR (simulating, say, the primary zone of an aircraft gas turbine combustor), we predict the resulting fraction evaporated, evaporation rate-controlled combustion "intensity", and corresponding exit droplet size distributions (DSD).
机译:我们在这里考虑了气相湍流对装有热压缩空气的绝热,充分搅拌的反应堆(WSR)中多分散稀燃料喷雾的蒸发动力学的影响。湍流增加了热扩散控制的液滴蒸发的时间平均速率,但由于液滴惯性和蒸发阻力的减小,增大因子取决于液滴的大小。因此,即使在相同的时间平均环境中,喷雾种群中的每个液滴也不会具有相同的面积变化率。当这些物理现象与表征WSR的停留时间分布(模拟飞机燃气轮机燃烧器的主要区域)相混淆时,我们预测了蒸发的分数,蒸发速率控制的燃烧“强度”以及相应的出口液滴大小分布(DSD)。

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