与航空声学系统啸叫频率变化有关的动力学状态

IF 4.3 2区 工程技术 Q1 ACOUSTICS Journal of Sound and Vibration Pub Date : 2024-07-06 DOI:10.1016/j.jsv.2024.118606
Ramesh S. Bhavi, Induja Pavithran, R.I. Sujith
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引用次数: 0

摘要

由流体动力场和声场相互作用产生的自持气声振荡被认为是一种啸叫。这种啸叫可导致大振幅声振荡,对大型分段式固体火箭发动机和大型天然气管道等工程系统造成灾难性后果。这种啸叫与动力系统理论中的极限周期振荡(LCO)状态相对应。当体积流速度作为控制参数变化时,气声系统会表现出不同的动力学状态。了解控制参数变化时的动力学状态及其之间的转换,对于设计针对此类气声振荡的控制策略至关重要。以往的研究表明,在流经孔道的气声系统中,随着控制参数的变化,啸叫频率也会发生变化。我们的研究表明,这种频率变化会通过三种不同的情况发生--(1) 两个 LCO 之间的直接过渡,即突然过渡;(2) 间歇状态;(3) 非周期性状态。在当前的气声系统中,LCO 之间的突然转换表现为爆裂行为,即声压波动的振幅在高振幅和低振幅 LCO 之间突然切换。此外,我们还表明,频移过程中的动态状态和它们之间的转换与频移的幅度有关。我们利用递推理论证明,在频移过程中,系统的动态状态会发生变化。此外,我们还利用同步理论研究了不同动力学状态下速度(u′)和声压(p′)波动的耦合行为。我们的研究结果表明,u′和 p′在 LCO 状态下表现出相位同步(PS),与啸叫相对应。相比之下,u′和 p′在非周期性状态下是不同步的,相当于稳定运行。此外,间歇期间的周期性振荡脉冲串对应于周期性 u′和 p′的相位同步历元,而非周期性历元对应于非同步的非周期性 u′和 p′。
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Dynamical states associated with the shift in whistling frequency in aeroacoustic system

Self-sustained aeroacoustic oscillations arising from the interactions between the hydrodynamic and acoustic fields are perceived as a whistle. Such whistling can lead to large amplitude acoustic oscillations that have disastrous consequences for engineering systems such as large segmented solid rocket motors and large gas pipelines. The whistling corresponds to the state of limit cycle oscillations (LCO) in dynamical systems theory. An aeroacoustic system exhibits different dynamical states when the bulk flow velocity is varied as a control parameter. Understanding the dynamical states and the transitions between them, as the control parameter is varied, is crucial in designing control strategies for such aeroacoustic oscillations. Previous studies have shown that as the control parameter varies, in an aeroacoustic system that has a flow through orifices, the whistling frequency shifts. We show that such a change in frequency occurs via three different scenarios— (1) direct transition between the two LCOs as an abrupt transition, (2) via a state of intermittency, and (3) via a state of aperiodicity. In the current aeroacoustic system, the abrupt transition between the LCOs is manifested as a bursting behaviour where the amplitude of the acoustic pressure fluctuations abruptly switches between the high and low-amplitude LCOs. Further, we show that the dynamical state and the transition between them during the frequency shift have a correlation with the magnitude of the frequency shift. Using recurrence theory we show that there is a change in the dynamical state of the system during the frequency shift. Further, we use synchronisation theory to investigate the coupled behaviour of the velocity (u) and the acoustic pressure (p) fluctuations during the different dynamical states. Our findings imply that u and p exhibit phase synchronisation (PS) during the state of LCO, corresponding to whistling. In contrast, u and p are desynchronised during the state of aperiodicity, corresponding to stable operation. Furthermore, the bursts of periodic oscillations during intermittency correspond to the phase-synchronised epochs of periodic u and p, and the aperiodic epochs correspond to the desynchronised aperiodic u and p.

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来源期刊
Journal of Sound and Vibration
Journal of Sound and Vibration 工程技术-工程:机械
CiteScore
9.10
自引率
10.60%
发文量
551
审稿时长
69 days
期刊介绍: The Journal of Sound and Vibration (JSV) is an independent journal devoted to the prompt publication of original papers, both theoretical and experimental, that provide new information on any aspect of sound or vibration. There is an emphasis on fundamental work that has potential for practical application. JSV was founded and operates on the premise that the subject of sound and vibration requires a journal that publishes papers of a high technical standard across the various subdisciplines, thus facilitating awareness of techniques and discoveries in one area that may be applicable in others.
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