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On Combustion Around a Porous Blowing Reactant Sphere in a Low Reynolds Number Crossflow

机译:低雷诺数错流下多孔反应物流球的燃烧

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The low Reynolds number limit of flow past a blowing reactant sphere serves to illustrate a powerful theoretical approximation for the conservation equations of combustion. For this approximation to work, the crossflow rate measured by the Reynolds number must be at least one order of magnitude smaller than the blowing Stefan flow rate from the porous sphere (droplet). This approximation, which retains in the equations only the irrotational component of the velocity field, enables analytical solutions to be derived for the mixture fraction and all other scalar variables. The mixture fraction solution permits predictions to be made for the flame including its shape and its position, and their dependence on both crossflow and radial sphere blowing. The porous sphere can also be treated as a transient, decaying fuel droplet in a quasi-steady gas. Using this simplification, an analytical droplet burning rate formula is derived and compared with an empirical correlation formula. Diffusion flame hole development is examined as a function of the crossflow.
机译:通过吹气反应物球体的低雷诺数极限表明了燃烧守恒方程的有力的理论近似。为了使这种近似起作用,用雷诺数测得的错流率必须至少比从多孔球体(液滴)吹出的斯蒂芬流率小一个数量级。该近似值仅将等式中的速度场的非旋转分量保留在方程中,从而可以导出混合分数和所有其他标量变量的解析解。混合分数解决方案允许对火焰进行预测,包括其形状和位置,以及它们对横流和径向球吹气的依赖性。多孔球体也可以被视为准稳态气体中的瞬变衰减燃料滴。通过这种简化,导出了分析液滴燃烧速率公式,并将其与经验相关公式进行比较。根据横流检查扩散火焰孔的发展。

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