Vortex Sound Models: Passive and Active Noise Control

Matthew J. Priddin, David I. Baker, Lorna J. Ayton, N. Peake
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引用次数: 4

Abstract

© 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Simple models of vortex sound, considering the motion of a line vortex past an object, have been used to determine the far-field noise due to an idealised hydrodynamic disturbance, modelling, for example, instabilities within a turbulent boundary layer. Extensions of such models to investigate devices designed for control of trailing-edge noise, both passively and actively, are proposed. This simple mathematical framework potentially gives insight into the mechanism behind experimentally observed reductions in far-field noise.
涡旋声模型:被动和主动噪声控制
©2018由美国航空航天研究所,Inc。版权所有。简单的涡旋声模型,考虑直线涡旋经过一个物体的运动,已经被用来确定由于理想的流体动力扰动引起的远场噪声,例如,湍流边界层内的不稳定性。提出了这些模型的扩展,以研究设计用于被动和主动控制尾缘噪声的设备。这个简单的数学框架可能会让我们深入了解实验观察到的远场噪声减少背后的机制。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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