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LARGE-EDDY SIMULATION AND LINEAR ACOUSTIC ANALYSIS OF A DIFFUSION SWIRLING FLAME UNDER FORCING AND SELF-EXCITATION

机译:强迫与自激旋转旋转火焰的大涡模拟和线性声学分析

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A diffusion swirling flame under external forcing and selfexcitation within a single swirler combustor have been studied in this paper with the large-eddy simulation and linear acoustic method. The combustor features pre-vaporized kerosene as the fuel, a single radial air swirler for flame stabilization and a square cross section chamber with adjustable length. Firstly, self-sustained pressure oscillation has been achieved by using of a chocked nozzle on the chamber outlet with large-eddy simulation. Dynamic pressure oscillations are analyzed in frequency domain through Fast Fourier Transform. The major pressure oscillation is identified as the 1st order longitudinal mode of the chamber. Further, the same frequency in the form of harmonic velocity oscillation is imposed on the inlet of the combustor while the chamber length has been changed. Based on this approach, a comparative study of the flame response with different excitation method but same frequency is carried out. In both self-excited and forced cases, global and local flame responses as well as Rayleigh index have been analyzed and compared. With the flame response function, the excited acoustic modes under the influence of dynamic heat release have been predicted with linear acoustic method and compared with the results obtained from large-eddy simulation. Results show that the flame response presents a great difference in the spacial distribution with different excitation approaches. Thermo-acoustic interaction distributes along the flame front with the expansion of the flame under self-excitation while it damps with the acoustic propagating downstream under forcing condition. As the ratio of flame length to acoustic wave length could not be neglected for the diffusion swirling flame, the global flame response under forcing cannot represent the local response feature of the flame accurately, thus influencing the instability prediction.
机译:本文研究了单旋流器燃烧器内的外部矫正和自我旋转下的扩散旋转火焰,具有大涡模拟和线性声学方法。燃烧器具有预蒸发的煤油作为燃料,用于火焰稳定的单个径向空气旋流器和具有可调节长度的方形横截面室。首先,通过使用大涡模拟的腔室出口上的Chocked喷嘴实现了自持续的压力振荡。通过快速傅里叶变换在频域中分析动态压力振荡。主压振荡被识别为腔室的第一阶纵向模式。此外,谐波速度振荡形式的相同频率施加在燃烧器的入口上,而腔室长度已经改变。基于这种方法,进行了不同励磁方法但相同频率的火焰响应的比较研究。在自我激发和强迫案例中,已经分析并比较了瑞利指数的全球和局部火焰反应。利用火焰响应函数,已经用线性声学方法预测了动态热释放的影响下的激发声模式,并与从大涡模拟获得的结果进行比较。结果表明,火焰响应呈现出不同励磁方法的空间分布差异。热声相互作用沿着火焰前沿分布,在自激动下膨胀火焰,同时抑制了在强迫条件下的下游的声学传播。随着扩散旋转火焰的扩散火焰不能忽略火焰长度与声波长度的比率,强迫下的全局火焰响应不能精确地表示火焰的局部响应特征,从而影响不稳定预测。

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