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首页> 外文期刊>Journal of low frequency noise, vibration and active control >Numerical studies of transmission loss performances of asymmetric Helmholtz resonators in the presence of a grazing flow
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Numerical studies of transmission loss performances of asymmetric Helmholtz resonators in the presence of a grazing flow

机译:放牧流动存在下不对称Helmholtz谐振器的传输损耗性能的数值研究

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As a typical noise-attenuating device, Helmholtz resonators are widely implemented in aero-engines and gas turbines to decrease the transmission of acoustic noise. However, an asymmetric Helmholtz resonator could be designed and implemented due to the limited space available in the engines. To examine and optimize the noise-attenuating performances of the asymmetric resonator, comparison studies are performed. For this, a two-dimensional frequency-domain model of a cylindrical duct with a grazing flow is developed. An asymmetric Helmholtz resonator is attached as a side branch. The model containing the linearized Navier-Stokes equations is validated first by comparing the predicted results with the experimental ones available in the literature. Further validation is conducted by comparing the results of an asymmetric resonator with the analytical ones available in the literature. The effects of (1) neck offset distance from the center of the resonator cavity denoted by e_c/a_s and (2) the grazing flow Mach number M_u are evaluated. It is shown that as the grazing flow Mach number is increased, the resonant frequencies and the maximum transmission losses are dramatically varied for a given e_c/a_s. As e_c/a_s is increased from 0 to 0.5 and M_u ≥ 0.1, the resonant frequencies and the maximum transmission losses are increased. However, when Mu is lower than 0.07, i.e. M_u≤0.07, the transmission loss performances are almost unchanged with e_c/a_s increased. The optimum design of the asymmetric resonator is shown to give rise to the resonant frequency being shifted by 10% and 2-5 dB more transmission loss at higher Mach number. Finally, visualization of vortex shedding formed at the neck of the asymmetric resonator confirms that acoustical energy is transformed into kinetic energy and absorbed by the surrounding air. This study opens up a numerical design approach to optimize an asymmetric resonator.
机译:作为典型的噪声衰减装置,Helmholtz谐振器广泛地在航空发动机和燃气轮机中实现,以降低声噪声的传动。然而,由于发动机中可用的有限空间,可以设计和实现不对称的亥姆霍兹谐振器。为了检查和优化非对称谐振器的噪声衰减性能,进行比较研究。为此,开发了具有放牧流程的圆柱形管道的二维频域模型。不对称Helmholtz谐振器作为侧枝附着。通过将预测结果与文献中可用的实验结果进行比较,首先验证包含线性化Navier-Stokes方程的模型。通过将非对称谐振器的结果与文献中可用的分析谐振器的结果进行比较来进行进一步的验证。 (1)颈部偏移距离来自谐振腔中心的颈部偏移距离由E_C / A_S和(2)的谐振腔和(2)所示的放牧流Mach编号M_U进行评估。结果表明,由于放牧流动马赫数增加,对于给定的E_C / A_S,谐振频率和最大传输损耗显着变化。由于E_C / A_S从0增加到0.5和M_U≥01.1,谐振频率和最大传输损耗增加。然而,当MU低于0.07时,即M_U≤0.07,e_c / a_s的传输损耗性能几乎不变。示出了不对称谐振器的最佳设计,以引起谐振频率在较高马赫数处移动10%和2-5dB的变速器损耗。最后,在非对称谐振器的颈部形成的涡旋脱落的可视化证实,声能被转化为动能并被周围的空气吸收。本研究开辟了一种数字设计方法来优化不对称谐振器。

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