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LES-FEM coupled analysis and experimental research on aerodynamic noise of the vehicle intake system

机译:进气系统空气动力噪声的LES-FEM耦合分析与实验研究

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摘要

To Thoroughly explore the aerodynamic noise in order to achieve a more efficient engineering application for a vehicle intake system, the large eddy simulation and the finite element method were employed in numerical simulations, and the aeroacoustic characteristics were validated through the experimental data. In this research, the k-epsilon model was adopted to simulate the steady state fluid dynamic, and the static pressure loss was consistent with the bench test data, indicating the computational fluid dynamics model was valid. After acquiring the data from the steady state simulation, the fluctuating pressure of the inner wall was calculated based on the transient state calculation results from the large eddy simulation. Thereafter, the finite element method was used to determine the acoustic performance of the intake system. By comparing the experiment data, the noise reduction indicated that the intake system performed well at various frequencies, e.g. 320 Hz, 520 Hz and 770 Hz, but poorly at 140 Hz, 210 Hz, 420 Hz and 600 Hz. Finally, the far-field aerodynamic noise was calculated based on FW-H equation, and the output showed that the noise of each measuring point agreed well with the test results in trend. In particular, the inlet sound pressure spectrum almost fit the test data with the airflow of 300 m(3)/h, and several amplitude peaks appeared at 210 Hz, 420 Hz and 600 Hz, corresponding to the low-attenuation region of the noise reduction curve. Moreover, the specific frequencies were not shifted with the airflow changing. In conclusion, the numerical simulation method proves to be effective in calculating the aerodynamic noise accurately. (C) 2016 Elsevier Ltd. All rights reserved.
机译:为了深入研究空气动力学噪声,以便在汽车进气系统中获得更有效的工程应用,在数值模拟中采用了大涡模拟和有限元方法,并通过实验数据验证了空气声学特性。本研究采用kε模型来模拟稳态流体动力学,其静压损失与台架试验数据一致,表明计算流体动力学模型是有效的。从稳态模拟中获取数据后,根据大涡模拟的瞬态计算结果,计算内壁的波动压力。此后,使用有限元方法确定进气系统的声学性能。通过比较实验数据,降噪表明进气系统在各种频率下(例如, 320 Hz,520 Hz和770 Hz,但在140 Hz,210 Hz,420 Hz和600 Hz时差。最后,根据FW-H方程计算了远场空气动力噪声,输出结果表明各测量点的噪声与试验结果吻合良好。特别是,进气声压谱几乎与气流300 m(3)/ h的测试数据吻合,并且在210 Hz,420 Hz和600 Hz处出现了几个幅度峰值,对应于噪声的低衰减区域。减少曲线。而且,特定频率没有随着气流的变化而移动。总之,数值模拟方法被证明可有效地准确计算空气动力噪声。 (C)2016 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Applied Acoustics》 |2017年第1期|107-116|共10页
  • 作者单位

    Zhejiang Univ, Coll Energy Engn, Hangzhou 310027, Zhejiang, Peoples R China;

    Zhejiang Univ, Coll Energy Engn, Hangzhou 310027, Zhejiang, Peoples R China;

    Zhejiang Univ, Coll Energy Engn, Hangzhou 310027, Zhejiang, Peoples R China;

    Hengbo Holdings Co Ltd, R&D Ctr, Taizhou 318000, Peoples R China;

    Zhejiang Met Environm Protect Design & Res Co Ltd, Hangzhou 310000, Zhejiang, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Aerodynamic noise; Large eddy simulation; FW-H equation; Intake system; Acoustic performance;

    机译:空气动力学噪声大涡模拟FW-H方程进气系统声学性能;

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