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Temporal and Spatiotemporal Analyses of Synchronization Transition in a Swirl-Stabilized Combustor

机译:旋流稳定燃烧室同步过渡​​的时空分析

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The coupled behavior of the acoustic pressure and the heat release rate fluctuations is studied in a swirl-stabilized combustor during the transition of system dynamics from combustion noise to thermoacoustic instability via intermittency. The framework of synchronization is used to analyze the temporal as well as the spatiotemporal behavior of these oscillations. The results of the synchronization transition observed in this combustor are further compared and contrasted with those recently reported by Pawar et al. ("Thermoacoustic Instability as Mutual Synchronization Between the Acoustic Field of the Confinement and Turbulent Reactive Flow," Journal of Fluid Mechanics, Vol. 827, Sept. 2017, pp. 664-693) and Mondal et al. ("Onset of Thermoacoustic Instability in Turbulent Combustors: An Emergence of Synchronized Periodicity Through Formation of Chimera-like States," Journal of Fluid Mechanics, Vol. 811, Jan. 2017, pp. 659-681) in a bluff-body stabilized combustor. A rigorous analysis of the synchronization transition of these oscillations in the frequency domain is also presented. The temporal analysis reveals that the synchronization states and the synchronization transition to thermoacoustic instability of the coupled acoustic pressure and heat release rate fluctuations are similar for both swirl-stabilized and bluff-body stabilized combustors. On the other hand, the spatiotemporal analysis of both the combustors during the state of strongly correlated periodic oscillations shows that, despite the acoustic power production being higher during this state, an increased amount of spatial incoherence is visible in the instantaneous and phase-conditioned phasor field of the reaction zone of the swirl-stabilized combustor as compared to that of the bluff-body stabilized combustor. In short, the present study unifies the synchronization transition of coupled oscillations in these turbulent combustors, wherein the mechanisms behind the onset of thermoacoustic instabilities are apparently different.
机译:在系统动力学从燃烧噪声到间歇性热声不稳定性的过渡过程中,研究了涡旋稳定燃烧室中声压和放热率波动的耦合行为。同步框架用于分析这些振荡的时间和时空行为。在此燃烧器中观察到的同步转变的结果与Pawar等人最近报道的结果进行了进一步的比较和对比。 (“作为限制空间的声场与湍流反应流之间的相互同步的热声不稳定性,”流体力学学报,第827卷,2017年9月,第664-693页)和Mondal等。 (“湍流燃烧器中热声不稳定性的开始:通过形成嵌合体状态形成同步周期,”《流体力学学报》,第811卷,2017年1月,第659-681页)在钝体中稳定的燃烧器。还提出了对这些振荡在频域中的同步转变的严格分析。时间分析表明,对于涡旋稳定和钝体稳定的燃烧器,耦合声压和放热率波动的同步状态和同步转变为热声不稳定性是相似的。另一方面,在强烈相关的周期性振荡状态下,两个燃烧器的时空分析表明,尽管在此状态下声功率产生较高,但在瞬时和相位条件相量中可见到空间不相干性增加与钝体稳定的燃烧器相比,涡流稳定的燃烧器的反应区的磁场强度更大。简而言之,本研究统一了这些湍流燃烧器中耦合振荡的同步转变,其中热声不稳定性产生的机制显然不同。

著录项

  • 来源
    《AIAA Journal》 |2019年第2期|836-847|共12页
  • 作者单位

    Indian Inst Technol Madras, Dept Aerosp Engn, Chennai 600036, Tamil Nadu, India;

    Indian Inst Technol Madras, Chennai 600036, Tamil Nadu, India|Amrita Vishwa Vidyapeetham, Dept Mech Engn, Kollam 690525, India;

    Indian Inst Technol Madras, Chennai 600036, Tamil Nadu, India|Potsdam Inst Climate Impact Res, D-14473 Potsdam, Germany;

    Indian Inst Technol Madras, Dept Aerosp Engn, Chennai 600036, Tamil Nadu, India;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
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