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Flow-Excited Acoustic Resonance Excitation Mechanism, Design Guidelines, and Counter Measures

机译:流动激发声共振激励机制,设计准则和对策

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The excitation mechanism of acoustic resonances has long been recognized, but the industry continues to be plagued by its undesirable consequences, manifested in severe vibration and noise problems in a wide range of industrial applications. This paper focuses on the nature of the excitation mechanism of acoustic resonances in piping systems containing impinging shear flows, such as flow over shallow and deep cavities. Since this feedback mechanism is caused by the coupling between acoustic resonators and shear flow instabilities, attention is focused first on the nature of various types of acoustic resonance modes and then on the aeroacoustic sound sources, which result from the interaction of the inherently unstable shear flow with the sound field generated by the resonant acoustic modes. Various flow-sound interaction patterns are discussed, in which the resonant sound field can be predominantly parallel or normal to the mean flow direction and the acoustic wavelength can be an order of magnitude longer than the length scale of the separated shear flow or as short as the cavity length scale. Since the state of knowledge in this field has been recently reviewed by Tonon et al. (2011, "Aeroacoustics of Pipe Systems With Closed Branches", Int. J. Aeroacoust., 10(2), pp. 201-276), this article focuses on the more practical aspects of the phenomenon, including various flow-sound interaction patterns and the resulting aeroacoustic sources, which are relevant to industrial applications. A general design guide proposal and practical means to alleviate the excitation mechanism are also presented. These are demonstrated by two examples of recent industrial case histories dealing with acoustic fatigue failure of the steam dryer in a boiling water reactor (BWR) due to acoustic resonance in the main steam piping and acoustic resonances in the roll posts of the Short Take-Off and Vertical Lift Joint Strike Fighter (JSF).
机译:声共振的激发机理早已为人所知,但该行业仍然受到其不良后果的困扰,这种不良后果在广泛的工业应用中表现为严重的振动和噪声问题。本文关注于包含冲击剪切流(例如浅腔和深腔)的管道系统中声共振激发机制的性质。由于此反馈机制是由声共振器和剪切流不稳定性之间的耦合引起的,因此首先应将注意力集中在各种类型的声共振模式的性质上,然后再关注由固有的不稳定剪切流的相互作用所导致的航空声源。共振声模产生的声场。讨论了各种流-声相互作用模式,其中共振声场可以主要平行于或垂直于平均流向,并且声波波长可以比分离的剪切流的长度尺度长一个数量级或短至腔体长度尺度。由于该领域的知识状态最近由Tonon等人进行了综述。 (2011年,“具有封闭分支的管道系统的航空声学”,Int。J. Aeroacoust。,第10卷第2期,第201-276页),本文着重研究了该现象的更实际方面,包括各种流-声相互作用模式和由此产生的空气声源,与工业应用有关。还提出了通用设计指南建议和减轻励磁机理的实用方法。这些通过最近的工业案例历史的两个例子得到了证明,这些案例历史涉及沸腾水反应堆(BWR)中的蒸汽干燥器的蒸汽疲劳故障,该蒸汽疲劳故障是由于主蒸汽管道中的声共振和短距离起飞的辊柱中的声共振引起的和垂直提升联合打击战斗机(JSF)。

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