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Scattering to Higher Harmonics for Quarter Wave and Helmholtz Resonators

机译:散射到四分之一波和亥姆霍兹谐振器的高次谐波

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The nonlinear response of acoustic resonators is investigated over a broad range of frequencies and amplitudes. Helmholtz resonators with a symmetric and with an asymmetric neck, respectively, as well as quarter wave resonators are considered. Describing functions for impedance and reflection coefficient of a Helmholtz resonator at various sound pressure levels are determined from compressible flow simulation and validated against experimental data. The particular focus of the present study is the nonlinear scattering to higher harmonics. For the Helmholtz resonator with a symmetric neck, a distinct pattern in the amplitudes of the higher harmonics is observed, where the odd harmonics dominate the response, while the even harmonics are almost negligible. Such an "Odd-Harmonics-Only" (OHO) pattern, which was observed previously in experiment at orifices, can be explained by a quasi-steady analysis based on the Bernoulli equation, assuming a symmetric flow pattern at the neck. For the Helmholtz resonator with an asymmetric neck, it is observed in CFD simulations that even harmonics contribute noticeably to the resonator response, such that the OHO pattern is less pronounced. For the markedly asymmetric geometry of the quarter wave resonator, the second harmonic is dominant and the OHO pattern vanishes completely. The quasi-steady analysis is extended successfully to describe also nonlinear scattering to higher harmonics for asymmetric configurations and flow patterns. Overall, the scattering to higher harmonics remains on a moderate level even at very high excitation levels for the Helmholtz resonator configurations. For the quarter wave resonator, the scattering is more pronounced and contributes perceptibly to the response at high excitation amplitudes.
机译:在很宽的频率和幅度范围内研究了声谐振器的非线性响应。考虑分别具有对称和不对称颈部的亥姆霍兹谐振器以及四分之一波长谐振器。根据可压缩流模拟确定了在各种声压级下亥姆霍兹谐振器的阻抗和反射系数的描述函数,并根据实验数据进行了验证。本研究的特别重点是对高次谐波的非线性散射。对于具有对称颈部的亥姆霍兹谐振器,可以观察到高次谐波幅度的独特模式,其中奇次谐波主导响应,而偶次谐波则几乎可以忽略不计。先前在孔口的实验中观察到的这种“仅奇次谐波”(OHO)模式可以通过基于伯努利方程的准稳态分析来解释,假设在颈部处为对称流动模式。对于具有不对称颈部的亥姆霍兹谐振器,在CFD仿真中观察到,即使谐波也对谐振器响应产生明显影响,因此OHO模式不太明显。对于四分之一波谐振器明显不对称的几何形状,二次谐波占主导地位,OHO模式完全消失。准稳态分析已成功扩展,以描述非对称配置和流型的非线性散射到高次谐波。总体而言,对于亥姆霍兹谐振器配置,即使在非常高的激励水平下,对高次谐波的散射仍保持在中等水平。对于四分之一波长谐振器,散射更为明显,并且在高激励振幅下明显地有助于响应。

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