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Computational aeroacoustic study of aircraft slat tracks and cut-outs

机译:计算气动声学研究飞机板条轨道和切口

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摘要

As one of the major contributors to aircraft noise, the noise generated by high-lift devices has been explored for many years. However, the noise related to the slat track system, which includes all the extrusive components connecting the slat and the main element, is still generally studied through experimentation due to the complex geometry. In this project, the aerodynamics and aeroacoustics of the slat track and cut-out, especially the main element cut-out, were investigated through numerical simulations for the first time. Two methods were employed in this work. Noise propagation is first studied via a compact source model to evaluate the contribution of each source individually and to investigate the influence of the slat track system on the noise propagation in the slat region. The APE-IV system was employed but modified by using a more accurate expression of enthalpy perturbation to calculate the acoustic fields. The results show that both the slat track system and the background flow modify the sound propagation path. The energy radiated towards the ground is increased due to the interaction of sound waves with the slat track system and the background flow. Detached eddy simulations were run to investigate the mechanisms of the slat track and cut-out noise generation. Major noise sources in the slat cove region are identified and a noise generation feedback loop is proposed. The results show that the increment of noise levels due to the existence of the slat track system is two-fold. The slat track and the cut-out generate noise individually and they also amplify the noise generated within the slat region when the sound waves propagate though the slat cove area and interact with the slat track and cut-out. The dominant frequencies of the spectrum are seen to shift towards the high frequencies due to these added on components. In this work, two kinds of possible noise attenuation approaches were proposed and studied. Geometries based on replacing the sharp cut-out on the main element leading edge with an edge-rounded or a sealed cut-out have been proved to be able to reduce the cut-out noise significantly. Application of acoustic bulk absorbing material can also attenuate the cut-out noise efficiently for a certain range of frequencies.
机译:作为飞机噪声的主要贡献者之一,高升力设备产生的噪声已经被研究了很多年。然而,由于复杂的几何形状,仍通常通过实验研究与板条轨道系统有关的噪声,该噪声包括连接板条和主要元件的所有挤压组件。在该项目中,首次通过数值模拟研究了板条轨道和切口,尤其是主要元素切口的空气动力学和空气声学特性。这项工作采用了两种方法。首先通过紧凑源模型研究噪声传播,以分别评估每个源的贡献,并研究板条轨道系统对板条区域噪声传播的影响。使用了APE-IV系统,但通过使用更精确的焓摄动表达式进行了修改以计算声场。结果表明,板条轨道系统和背景流均会改变声传播路径。由于声波与板条轨道系统和背景流的相互作用,向地面辐射的能量增加了。进行了分离涡流仿真,以研究板条轨道和切出噪声产生的机理。确定了板条湾区域的主要噪声源,并提出了噪声产生反馈回路。结果表明,由于板条轨道系统的存在,噪声水平的增加是两倍。板条轨道和切口分别产生噪声,并且当声波传播通过板条湾区域并与板条轨道和切口相互作用时,它们还会放大板条区域内产生的噪声。由于在组件上增加了这些频率,因此可以看出频谱的主频向高频移动。在这项工作中,提出并研究了两种可能的噪声衰减方法。事实证明,通过将主元件前缘上的尖锐切口替换为圆角或密封切口,可以大大降低切口噪声。吸声体吸收材料的应用还可以在一定频率范围内有效衰减切出的噪声。

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  • 作者

    Wang Xin;

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  • 年度 2013
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  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"English","id":9}
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