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Response of a laminar premixed V-flame to a high-frequency transverse acoustic field

机译:层流预混V型火焰对高频横向声场的响应

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This work presents new results describing the action of an acoustic transverse standing wave on a methane-air premixed V-flame located at a pressure antinode. Investigations of the jet highlight a mode conversion from a transverse cavity mode to a longitudinal mode, involving a "plugging" flow-rate modulation. This essential mechanism generates vortical structures convected toward the flame stabilized on a vertical rod introduced inside the burner and aligned with its axis. Depending on acoustic conditions, they develop through one of the following patterns: a pairing process, a multiple-vortex interaction in the jet outer layer, or a helical mode in the inner layer behind the rod. The flame responses are arranged in the physical space defined by the acoustic pressure amplitude (P_(ref)) and the Strouhal numbers, St characteristic of the dominant (outer or inner) shear-layer. A harmonic flame response at the forcing frequency, f_0, is not the only possible behavior. The other behaviors observed are an asymmetrical "elongated wrinkled flame" due to the helical mode; an "aperiodic fluctuating flame"; and a "sub-harmonic rolled-up flame" due to the pairing process, which induces strong CH~* emission fluctuations at f_0/2. Several flame dynamics evolutions are noted when P_(ref) increases. The heat release rate (h.r.r.) always begins to fluctuate at f_0. Then, depending on St, it can undergo the nonlinear frequency bifurcation; and next, it may fluctuate at f_0 again in addition to f_0/2. Another scenario shows the h.r.r. losing any kind of ordered modulation before it eventually fluctuates at f_0. The flame stabilization is described at blowout via the leading edge behavior. Foot-displacement amplitude, and foot-width thinning and straightening are complementary dynamics and morphology features that characterize flame destabiliza-tion. The different patterns, observed as P_(ref) increases, of successive ordered flame responses, sometimes alternating with aperiodic responses, appear as the main elements in understanding the processes involved in thermoacoustic instabilities.
机译:这项工作提出了新的结果,描述了声横驻波对位于压力波腹处的甲烷-空气预混V型火焰的作用。对射流的研究突出了从横向腔模式到纵向模式的模式转换,涉及“堵塞”流量调制。这种基本的机制产生的涡流结构朝着火焰对流,涡流结构稳定在引入燃烧器内部并与其轴线对齐的垂直杆上。根据声学条件,它们通过以下模式之一发展:配对过程,射流外层中的多涡旋相互作用或杆后内层中的螺旋模式。火焰响应布置在由声压幅度(P_(ref))和主要(外部或内部)剪切层的Strouhal数,St特性定义的物理空间中。强制频率f_0上的谐波火焰响应不是唯一可能的行为。观察到的其他行为是由于螺旋模式引起的不对称“伸长的皱纹火焰”。 “非周期性波动的火焰”;以及由于配对过程产生的“次谐波卷起火焰”,在f_0 / 2处会引起强烈的CH〜*发射波动。当P_(ref)增加时,会注意到一些火焰动力学演变。放热率(h.r.r.)始终在f_0处开始波动。然后,根据St,它会经历非线性分频;接下来,除了f_0 / 2以外,它可能还会在f_0处波动。另一种情况显示人力资源状况。失去任何有序调制,直到它最终在f_0波动。通过前缘行为描述了喷火时的火焰稳定度。脚位移幅度以及脚宽度变薄和变直是火焰不稳定的互补动力学和形态特征。随着P_(ref)的增加,观察到的不同模式是连续有序火焰响应(有时与非周期性响应交替出现),是理解热声不稳定性过程的主要元素。

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