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Computational Acoustic Beamforming of Noise Source on Wind Turbine Airfoil

机译:风力机翼型噪声源的计算声波束形成

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摘要

A new method, Computational Acoustic Beamforming, is proposed in this thesis. This novel numerical sound source localization methodology combines the advantages of the Computational Fluid Dynamics (CFD) simulation and experimental acoustic beamforming, which enable this method to take directivity of sound source emission into account while maintaining a relatively low cost. This method can also aid the optimization of beamforming algorithm and microphone array design. In addition, it makes sound source prediction of large structures in the low frequency range possible.Three modules, CFD, Computational Aeroacoustics (CAA) and acoustic beamforming, are incorporated in this proposed method. This thesis adopts an open source commercial software OpenFOAM for the flow field simulation with the Improved Delayed Detached Eddy Simulation (IDDES) turbulence model. The CAA calculation is conducted by an in-house code using impermeable Ffowcs-Williams and Hawkings (FW-H) equation for static sound source. The acoustic beamforming is performed by an in-house Delay and Sum (DAS) beamformer code with several different microphone array designs.Each module has been validated with currently available experimental data and numerical results. A flow over NACA 0012 airfoil case was chosen as a demonstration case for the new method. The aerodynamics and aeroacoustics results are shown and compared with the experimental measurements. A relatively good agreement has been achieved which gives the confidence of using this newly proposed method in sound source localization applications.
机译:本文提出了一种计算声波束形成的新方法。这种新颖的数值声源定位方法结合了计算流体力学(CFD)模拟和实验声束形成的优点,使该方法能够在保持相对较低成本的同时考虑声源发射的方向性。该方法还可以帮助优化波束形成算法和麦克风阵列设计。此外,它还可以在低频范围内对大型结构进行声源预测。该方法结合了CFD,计算航空声学(CAA)和声束成形三个模块。本文采用改进的延迟分离涡模拟(IDDES)湍流模型,采用开源商业软件OpenFOAM进行流场仿真。 CAA计算是通过内部代码使用静态声源的不渗透Ffowcs-Williams和Hawkings(FW-H)方程进行的。声学波束形成由内部延迟和加和(DAS)波束形成器代码执行,具有几种不同的麦克风阵列设计,每个模块均已通过当前可用的实验数据和数值结果进行了验证。选择了NACA 0012机翼外壳上方的气流作为新方法的演示案例。显示了空气动力学和空气声学结果,并与实验测量结果进行了比较。已经达成了相对较好的协议,这给了在声源定位应用中使用这种新提出的方法的信心。

著录项

  • 作者

    Li Chi Shing;

  • 作者单位
  • 年度 2014
  • 总页数
  • 原文格式 PDF
  • 正文语种 en
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