压力梯度对火焰-涡相互作用及火焰稳定性的影响

Yagiz Yalcinkaya, O. E. Bozkurt, A. G. Gungor
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引用次数: 0

摘要

本文对紊流预混崖体稳定火焰进行了数值研究,强调了压力梯度对火焰-涡相互作用和稀薄燃烧火焰稳定性的影响。提出了四种不同几何结构的大涡模拟,扩压器3°,扩压器1.5°,标称和喷嘴,导致轻微到强烈的压力梯度。数值研究允许确定几何诱导的压力梯度对火焰结构、火焰前涡度和湍流结构的发展以及火焰稳定的影响。结果表明,压力梯度对火焰锋面涡度和斜压转矩的时空发展起着关键作用。扩散器几何形状中的流动减速抑制了火焰诱导涡度机制,这反过来导致火焰的大褶皱形式,并可能导致沿火焰锋面的局部消失。相反,喷嘴几何形状中的有利压力梯度增加了斜压扭矩,从而抑制了剪切层涡度的发展,从而防止了局部消失。
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Influence of Pressure Gradient on Flame-Vortex Interaction and Flame Stability
This study presents numerical investigations of turbulent premixed bluff-body stabilized flame by emphasizing the influence of pressure gradient on flame-vortex interaction and flame stability for lean combustion applications. Large eddy simulations of four different geometrical configurations, diffuser 3°, diffuser 1.5°, nominal, and nozzle that resulted in mild to strong pressure gradients are presented. Numerical investigations allowed determining the effects of geometry-induced pressure gradient on the flame structure, development of the flame-front vorticity and turbulent structures and flame stabilization. It is shown that the pressure gradient plays a key role for the spatial and temporal development of the flame front vorticity and baroclinic torque. The flow deceleration in diffuser geometries suppresses the flame-induced vorticity mechanisms, which in turn lead to large wrinkle forms of the flame and may lead to local extinctions along the flame front. The favorable pressure gradient in the nozzle geometry, on the contrary, increases the baroclinic torque that restrains the development of the shear layer vorticity and hence prevents local extinctions.
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