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Simulating the nonlinear acoustic oscillations in a resonator by gas-kinetic scheme

机译:用气体动力学方法模拟谐振器中的非线性声振荡

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The nonlinear oscillation in a compressible air-filled two-dimensional cylindrical resonator driven by a loudspeaker is simulated by using the gas-kinetic scheme. The influences of shock wave and higher harmonic on the time and space distribution of acoustic variables are investigated numerically for the practical applications of high-intensity acoustic devices. The validation of the developed model is verified by comparing the numerical results of pressure distribution with the theoretical ones for the finite-amplitude case. And then, the verified gas-kinetic scheme is used to simulate the acoustic field of highly nonlinear standing wave. Some interesting physical phenomena have been revealed for the highly nonlinear case. Sharp velocity spikes accompanied by the saw-tooth pressure waveforms appear at the end of the resonator. Moreover, the pressure at the position of theoretical pressure node is not zero and its frequency is about twice of the resonance frequency. Furthermore, the second harmonic is predominant at the location of pressure node. And nonlinear saturation can be found in tandem as the shock wave appears. Additionally, quasi-one-dimensional distribution accompanied changing flow direction and annular effect is observed for the spatial distribution of x-velocity. In addition, the y-velocity is in an irregular two-dimensional distribution and the y-velocity is not any more negligible relative to the x-velocity. Meanwhile, the important impacts as well as the causes of these nonlinear phenomena are analyzed. The results demonstrate the gas-kinetic scheme is an efficient and appropriate method for simulation of highly nonlinear acoustic oscillation and concerned problems. (C) 2014 Elsevier Inc. All rights reserved.
机译:利用气体动力学方法,模拟了扬声器驱动的可压缩充气二维圆柱谐振器的非线性振荡。数值研究了冲击波和高次谐波对声学变量的时间和空间分布的影响,以用于高强度声学设备的实际应用。通过将压力分布的数值结果与有限振幅情况下的理论结果进行比较,验证了所开发模型的有效性。然后,使用已验证的气体动力学方案来模拟高度非线性驻波的声场。对于高度非线性的情况,已经揭示了一些有趣的物理现象。共振器末端出现尖锐的速度峰值,并伴随有锯齿形的压力波形。此外,理论压力节点处的压力不为零,其频率约为共振频率的两倍。此外,二次谐波主要在压力节点的位置。随着冲击波的出现,非线性饱和可以同时发现。此外,对于x速度的空间分布,观察到伴随流动方向变化和环形效应的准一维分布。此外,y速度呈不规则的二维分布,并且相对于x速度,y速度不再可忽略不计。同时,分析了这些非线性现象的重要影响及其成因。结果表明,气体动力学方案是一种用于仿真高度非线性声振荡和相关问题的有效且合适的方法。 (C)2014 Elsevier Inc.保留所有权利。

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