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Prediction and control of sound propagation in turbofan engine bypass ducts

机译:涡扇发动机旁通管声传播的预测与控制

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摘要

This thesis contains original research into the propagation of sound in acoustically lined ducts with flow. The motivation for this work is the requirement to predict the sound attenuation of acoustic liners in the bypass duct of modern turbofan aeroengines. The liners provide the most effective means with which to suppress the rear fan noise. It is therefore important to make the best possible use of the available lined area by optimising the liner configuration. A set of analytic and numerical methods for predicting the liner attenuation performance have been developed, which are suitable for use in intensive liner optimisation studies, or as preliminary design tools. Eigenvalue solvers have been developed to find modal solutions in rectangular ducts with uniform flow and annular ducts with sheared flow. The solvers are validated by replicating results from the scientific literature and the Finite Element method. The effect of mean core flow radial profile and boundary layers on the mode eigenfunctions and axial decay rates are considered. It is shown that solutions for thin boundary layer flows converge to those based on the commonly used slip flow boundary condition. It is demonstrated that realistic flow profiles should be used to assess acoustic mode propagation in bypass ducts. The flow profile can have strong effects upon low order modes and surface waves, and in fact at high frequencies, the profile can affect all the modes. Mode-matching schemes are developed to assess the power attenuation performance and modal scattering of finite length liners. The results of the schemes are used to show that refraction of sound by boundary layers increases attenuation at high frequency. Power attenuation is higher where the mean core flow gradient refracts sound towards the liner. It is found that asymmetric liners can provide improved attenuation, depending on the direction of the mean flow shear gradient. The optimisation of axially-segmented liners for single and multi-mode sources is demonstrated. It is found that potentially large improvements in the attenuation of tonal noise is possible, whilst benefits for broadband noise are more difficult to achieve.
机译:本论文包含有关在带有流动的隔声管道中传播声音的原始研究。开展这项工作的动机是需要预测现代涡轮风扇航空发动机旁路管道中的隔音衬里的声音衰减。衬里提供了抑制后风扇噪音的最有效方法。因此,重要的是通过优化衬里配置来最大程度地利用可用的衬里区域。已经开发了一套用于预测衬管衰减性能的解析和数值方法,适合用于密集的衬管优化研究或用作初步设计工具。特征值求解器已经开发出来,可以在均匀流动的矩形管道和剪切流动的环形管道中找到模态解。通过复制科学文献和有限元方法的结果来验证求解器。考虑了平均岩心流径向剖面和边界层对振型特征函数和轴向衰减率的影响。结果表明,薄边界层流的解收敛于基于常用滑流边界条件的解。结果表明,应使用实际的流量剖面来评估旁路管道中的声模传播。流动剖面对低阶模态和表面波会产生强烈影响,实际上,在高频下,剖面会影响所有模态。开发了模式匹配方案以评估有限长度衬管的功率衰减性能和模式散射。方案的结果用于表明边界层对声音的折射会增加高频下的衰减。在平均堆芯流动梯度使声音向内衬折射的情况下,功率衰减会更高。发现不对称衬里可以提供改善的衰减,具体取决于平均流量剪切梯度的方向。演示了针对单模和多模源的轴向分段衬套的优化。已经发现,可能在音调噪声的衰减方面有很大的改进,而更难获得宽带噪声的好处。

著录项

  • 作者

    Brooks Christopher James;

  • 作者单位
  • 年度 2007
  • 总页数
  • 原文格式 PDF
  • 正文语种 English
  • 中图分类

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