强迫方向对稀燃喷雾火焰传递函数的影响

N. Treleaven, A. Fischer, Claus Lahiri, M. Staufer, A. Garmory, G. Page
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引用次数: 1

摘要

采用大涡模拟(LES)方法计算了工业稀燃喷油器的火焰传递函数(FTF),并与多传声器技术和OH*测量的实验结果进行了比较。火焰传递函数将燃烧室放热的波动与喷油器气流的波动联系起来,是燃烧系统热声分析的重要组成部分。多传声器法通过在声学上强迫火焰从上游和下游交替产生FTF。利用可压缩大涡模拟(LES)完成了对该方法的模拟。这些模拟还可以直接通过测量质量流率和热释放率的波动来推导出FTF,从而将每个频率的模拟次数减少到1次,大大降低了模拟成本。从下游进行的声强迫模拟结果显示,与从上游进行的模拟相比,从上游进行的声强迫模拟产生的FTF增益值较低,且相位变化较小,这与理论一致。通过使用稍微不同的FTF定义,这也被证明与使用OH*化学发光测量的热释放率一致,但这些结果与多麦克风方法的结果不一致。这种差异来自于没有对喷油器出口平面的声阻抗进行精确测量,以及某些对流现象,这些现象改变了下游的速度和压力场,相对于纯声信号。所有仿真结果都表明,该滤波器的增益低于实验,但相位再现良好。先前的工作表明,这种误差可能是由于声强迫引起的燃料喷雾雾化过程的波动造成的,而这在本研究中没有建模。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The Effects of Forcing Direction on the Flame Transfer Function of a Lean-Burn Spray Flame
The flame transfer function (FTF) of an industrial lean-burn fuel injector has been computed using large eddy simulation (LES) and compared to experimental measurements using the multi-microphone technique and OH* measurements. The flame transfer function relates the fluctuations of heat release in the combustion chamber to fluctuations of airflow through the fuel injector and is a critical part of thermoacoustic analysis of combustion systems. The multi-microphone method derives the FTF by forcing the flame acoustically, alternating from the upstream and downstream side. Simulations emulating this methodology have been completed using compressible large eddy simulations (LES). These simulations are also used to derive an FTF by measuring the fluctuations of mass flow rate and heat release rate directly which reduces the number of simulations per frequency to one, significantly reducing the simulation cost. Simulations acoustically forced from downstream are shown to result in a lower value of the FTF gain than simulations forced from upstream with a small change in phase, this is shown to be consistent with theory. Through using a slightly different definition of the FTF, this is also shown to be consistent with measurements of the heat release rate using OH* chemiluminescence however these results are inconsistent with the multi-microphone method result. The discrepancy comes from not having an accurate measurement of the acoustic impedance at the exit plane of the injector and from certain convective phenomena that alter the downstream velocity and pressure field with respect to the purely acoustic signal. All simulations show a lower gain in the FTF than the experiments but with good reproduction of phase. Previous work suggests this error is likely due to fluctuations of the fuel spray atomisation process due to the acoustic forcing which is not modelled in this study.
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