镂空尾翼宽频气动噪声降噪研究

Research on noise reduction for broadband aeroacoustic noise of hollow roof spoilers

  • 摘要: 作为乘用车尾部重要的造型外饰件,镂空尾翼在高速行驶工况易产生宽频噪声问题,影响二排乘员的舒适性体验。针对该问题,本研究采用格子玻尔兹曼方法和统计能量分析方法,对镂空尾翼宽频气动噪声开展特性分析与降噪优化研究。分析结果表明,在250~1000 Hz频段,气动噪声主要由支架处旋涡脱落、尾翼前缘气流分离及后缘旋涡脱落现象诱导产生;在20004000 Hz频段,噪声主要来自尾翼前缘。通过优化尾翼前缘型面与支架型面、控制镂空通道面积,可有效减弱宽频噪声的影响,仿真结果显示优化方案可将二排语音清晰度恶化量降低6.3个百分点,并通过风洞试验验证了优化方案的有效性。本研究可为乘用车镂空尾翼宽频气动噪声降噪优化设计提供指导。

     

    Abstract: The hollow roof spoiler, a key rear-exterior styling component of passenger vehicles, tends to generate broadband aeroacoustic noise when the vehicle travels at elevated speeds, thereby compromising the acoustic comfort of second-row occupants. To address this issue, the present study integrates the lattice-Boltzmann method (LBM) with statistical energy analysis (SEA), and performs a systematic characterization and optimisation of the broadband aeroacoustic noise radiated by the hollow roof spoiler. The analysis demonstrates that, in the 250-1000  Hz frequency band, the dominant noise mechanisms involve vortex shedding from the supporting brackets, flow separation at the spoiler’s leading edge, and vortex shedding from the trailing edge, while in the 2000-4000  Hz frequency band, the noise is principally contributed by the leading-edge region of the spoiler. By refining the leading-edge contour of the spoiler, reshaping the geometry of the support structure, and regulating the hollow area, the broadband noise level can be markedly reduced. Numerical simulations indicate that the optimized configuration reduces the deterioration in articulation index for the second-row passengers by 6.3 percentage points. Wind-tunnel tests conducted under representative operating conditions validate the effectiveness of the proposed design modifications. Consequently, this work provides practical design guidelines for the mitigation and optimization of broadband aeroacoustic noise produced by hollow roof spoilers in passenger-vehicle applications.

     

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