首页> 外文期刊>Journal of Sound and Vibration >Using large eddy simulation to explore sound-source mechanisms in jets
【24h】

Using large eddy simulation to explore sound-source mechanisms in jets

机译:使用大型涡流模拟探索喷气机的声源机理

获取原文
获取原文并翻译 | 示例
           

摘要

This paper presents an analysis of data generated by means of large eddy simulation for a single-stream, isothermal Mach 0.9 jet. The acoustic field is decomposed into Fourier modes in the azimuthal direction, and filtered by means of a continuous wavelet transform in the temporal direction. This allows the identification of temporally localised, high-amplitude events in the radiated sound field for each of the azimuthal modes. Once these events have been localised, the flow field is analysed so as to determine their cause. Results show high-amplitude, intermittent sound radiation for azimuthal modes 0 and 1. The mode-0 radiation, which dominates low-angle emission, is found to result from the temporal modulation of a basic axisymmetric wave-packet structure within the flow. Similar intermittent activity, observed, again within the flow, for azimuthal mode 1 suggests a link between the modes 0 and 1 dynamics. Both the amplitude and spatial extent of the axisymmetric wave-packet are modulated, and the strongest axisymmetric propagative disturbances are found to radiate from the downstream end of the wave-packet at moments when the wave envelope becomes truncated. The observed behaviour is modelled using a line-source wave-packet ansatz which includes parameters that account for the said modulation. Inclusion of these parameters, which allow the wave-packet to jitter in a manner similar to that observed, leads to good quantitative agreement (accurate to within 1.5 dB), at low emission angles, with the acoustic field of the LES. This result is in contrast with results obtained using a time-averaged wave-packet (one which does not jitter), for which a 12 dB error is observed. This result shows that the said modulations are the salient source feature for the low-angle sound emission of the jet considered. Analysis of a longer time series shows the occurrence of several similar high-amplitude bursts in the axisymmetric mode of the acoustic pressure, and a calculation of the radiated sound for this longer time-series, again using the wave-packet ansatz, once again leads to good agreement with the LES (now accurate to within 1 dB).
机译:本文介绍了对单流等温Mach 0.9射流通过大涡流模拟生成的数据的分析。声场在方位方向上分解为傅立叶模式,并通过在时间方向上的连续小波变换进行滤波。这允许针对每个方位模识别辐射声场中的时间局部的高振幅事件。一旦确定了这些事件,便会分析流场以确定其原因。结果显示了0和1方位角模式的高振幅,间歇声辐射。发现模式0辐射主要是低角度发射,它是由流中基本轴对称波包结构的时间调制引起的。在方位角模式1中,再次在流中观察到类似的间歇活动,表明模式0和1动力学之间存在联系。轴对称波包的幅度和空间范围都得到了调制,并且在波包络被截断的时刻,从波包的下游端辐射出最强的轴对称传播干扰。使用线源波包ansatz对观察到的行为进行建模,该源包括其解释所述调制的参数。包含这些参数,可以使波包以类似于观察到的方式抖动,从而在低发射角处与LES的声场产生良好的定量一致性(精确到1.5 dB以内)。该结果与使用时间平均波包(不抖动)获得的结果相反,该时间包观察到12 dB的误差。该结果表明,所述调制是所考虑的射流的低角度声发射的显着源特征。对较长时间序列的分析显示,在声压的轴对称模式下,出现了多个类似的高振幅猝发,并再次使用波包ansatz计算了该较长时间序列的辐射声,这再次导致与LES(现在精确到1 dB以内)的良好一致性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号