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REDUCTION OF INTERIOR SOUND FIELDS IN FLEXIBLE CYLINDERS BY ACTIVE VIBRATION CONTROL

机译:通过主动振动控制减少柔性气缸中的内部声场

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An analytical model of a thin, flexible shell is evaluated to study the mechanisms of interior sound reduction by active control of the shell vibrational response. A single exterior acoustic monopole is used as the noise source while the secondary controller is represented as a single point force applied directly to the shell wall. The complex amplitude of the acoustic monopole is specified a priori, however, the complex amplitude of the point controller is initially unknown. The control force amplitude is evaluated such that the line-weighted mean square pressure is minimized along the shell wall in the excitation plane. The active control model is evaluated for harmonic excitation. Results indicate spatially averaged noise reductions in excess of 20 dB over the source plane for acoustic resonant conditions within the cavity. Modal response of the shell and the coupled interior pressure field indicate substantial control spillover in the shell due to control force excitation; however, control spillover is predominately constrained to the shell and thus does not contaminate the contained acoustic field.
机译:评估薄,柔性壳的分析模型,以研究通过主动控制壳振动响应的内部声音减少机制。单个外声学单极单极用作噪声源,而辅助控制器表示为直接施加到壳壁的单点力。声学单极的复幅度被指定为先验,然而,点控制器的复幅最初是未知的。评估控制力幅度,使得线加权均方压力沿着激发平面中的壳壁最小化。评估主动控制模型以进行谐波激发。结果表明在腔体内的声源平面上超过20dB的空间平均噪声减少。壳体和耦合内部压力场的模态响应表示由于控制力激发而在外壳中的大量控制溢出;然而,控制溢出物主要被限制在壳体上,因此不会污染包含的声场。

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