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Corner Vortex Structures: Spanwise Imaging of a Confined, Premixed Bluff-Body-Stabilized Flame

机译:角涡结构:密闭,预混的钝体稳定火焰的横向成像

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摘要

Large-scale corner vortex structures (CVS) are observed experimentally inside the recirculation zone of a confined, turbulent, premixed, two-dimensional bluff-body-stabilized flame. These counter-rotating CVS contribute to spanwise non-uniformity of the recirculation zone velocity field under reacting conditions but are not present for non-reacting conditions. To investigate the structure and dynamics of the CVS, experiments are performed that vary the fuel type (propane vs. natural gas), inlet velocity, preheat temperature, equivalence ratio, and bluff-body aspect ratio. As equivalence ratio is decreased from stoichiometric to lean blowout (LBO), the vorticity and circulation of the CVS increase, and the combustion on the spanwise plane becomes increasingly non-uniform. During the LBO process, the CVS are the final regions to sustain reactions. Simulations or measurements of bluff body stabilized flames which neglect the vortices in the spanwise plane may fail to capture both stable and LBO combustion processes. These effects of corner vortex structures and spanwise nonuniformity should be considered in future experimental and computational studies of confined bluff body-stabilized flames.
机译:在密闭的,湍流的,预混合的二维钝体稳定火焰的再循环区内,实验观察到了大规模的角涡结构(CVS)。这些反向旋转的CVS导致在反应条件下回流区速度场的展向分布不均匀,但在非反应条件下则不存在。为了研究CVS的结构和动力学,进行了改变燃料类型(丙烷与天然气),进气速度,预热温度,当量比和钝体长径比的实验。随着当量比从化学计量比变为稀薄喷出(LBO),CVS的涡旋和循环增加,并且在翼展方向上的燃烧变得越来越不均匀。在杠杆收购过程中,CVS是维持反应的最后区域。忽略翼展方向平面中的涡流的钝体稳定火焰的模拟或测量可能无法捕获稳定燃烧过程和LBO燃烧过程。在未来的受限钝体稳定火焰的实验和计算研究中,应考虑角涡结构和翼展方向不均匀性的这些影响。

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