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Sidewall controlling large-scale flow structure and reversal in turbulent Rayleigh-Bénard convection 侧壁控制湍流Rayleigh-Bénard对流中的大尺度流动结构和逆转
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-06-03 DOI: 10.1080/14685248.2021.1916023
J. Cheng, Jianzhao Wu, Yu-lu Liu, Zhiming Lu
Spontaneous and stochastic reversal of large scale flow structure is an intriguing and crucial phenomenon in turbulent Rayleigh-Bénard type natural convection. This paper proposes a new control approach to eliminate the reversals through stabilising the corner flows using two small sidewall controllers. Based on a series of direct numerical simulations, it is shown that the control can successfully stop the growth of corner vortices and suppress the reversal of large-scale circulation, if the width of sidewall controllers installed within or near the top of corner vortices is large enough. When the controllers are located around the centre, they can easily break up the large-scale structures or even divide the single roll mode into a double-roll mode for very large widths. Moreover, the influence of sidewall controllers on the heat transport is studied. It is shown that the heat transport efficiency can be slightly enhanced or suppressed when the proper location and width are chosen. The present findings provide a new idea to control the large-scale flow structure and reversals in thermally driven convection through sidewall controlling.
在湍流Rayleigh-Bénard型自然对流中,大尺度流动结构的自发和随机逆转是一个有趣而关键的现象。本文提出了一种新的控制方法,通过使用两个小型侧壁控制器稳定角流来消除反向。基于一系列直接数值模拟,结果表明,如果安装在角涡顶部或附近的侧壁控制器的宽度足够大,该控制可以成功地阻止角涡的增长,并抑制大规模环流的逆转。当控制器位于中心附近时,它们可以很容易地分解大型结构,甚至可以将单辊模式划分为双辊模式,以获得非常大的宽度。此外,还研究了侧壁控制器对热传输的影响。结果表明,当选择合适的位置和宽度时,热传输效率可以略有提高或抑制。本研究结果为通过侧壁控制来控制大规模流动结构和热驱动对流的逆转提供了一种新的思路。
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引用次数: 1
Development of an intermittency transport equation for modeling bypass, natural and separation-induced transition 建立了用于模拟旁路、自然和分离诱导过渡的间歇性输运方程
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-06-03 DOI: 10.1080/14685248.2021.1932947
E. Juntasaro, K. Ngiamsoongnirn, Phongsakorn Thawornsathit, P. Durbin
ABSTRACT The objective of this paper is to propose a new intermittency transport equation that is naturally capable of capturing the effects of free-stream turbulence and pressure gradient on bypass and natural transition without need for any extra parameters/terms to take into account the free-stream turbulence and the pressure gradient. This new intermittency transport equation is obtained by derivation and, in it, only its production term is modeled via two empirical functions in order to detect the onset location of transition and to control the growth rate of transition process. Only one sensing parameter is used to detect the transition onset for both natural and bypass transition. For the purpose of not altering the original form of the base turbulence model, the effective intermittency factor is used to describe the separation-induced transition. The base turbulence model remains unmodified in conjunction with the effective intermittency factor as a regulator to control the net turbulent generation rate. For the evaluation of model performance, the modeled intermittency equation is tested against (1) the transitional boundary layer on a flat plate with zero and non-zero pressure gradients, (2) the transitional flow over a compressor blade with a laminar separation bubble, and (3) the transitional flow over a wind turbine airfoil at various angles of attack. The present results are also compared to those of the transition model of Menter et al. [1] and those of the transition model of Langtry and Menter [2]. The evaluation results reveal that the new intermittency transport equation is capable of predicting the bypass, natural and separation-induced transition.
摘要本文的目的是提出一种新的间歇性输运方程,该方程能够自然地捕捉自由流湍流和压力梯度对旁路和自然过渡的影响,而不需要任何额外的参数/项来考虑自由流紊流和压力梯度。这个新的间歇输运方程是通过推导得到的,其中只有它的产生项通过两个经验函数建模,以检测过渡的起始位置并控制过渡过程的增长率。仅使用一个感测参数来检测自然过渡和旁路过渡的过渡开始。为了不改变基础湍流模型的原始形式,使用有效间歇因子来描述分离诱导的跃迁。基础湍流模型与有效间歇因子一起保持不变,作为控制净湍流产生率的调节器。为了评估模型性能,针对(1)具有零和非零压力梯度的平板上的过渡边界层,(2)具有层流分离气泡的压缩机叶片上的过渡流,以及(3)不同迎角下的风力涡轮机翼型上的过渡流动,对建模的间歇方程进行了测试。本结果还与Menter等人[1]的过渡模型以及Langtry和Menter[2]的过渡模型的结果进行了比较。评价结果表明,新的间歇输运方程能够预测旁路、自然和分离诱导的跃迁。
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引用次数: 4
Honeycomb-generated Reynolds-number-dependent wake turbulence 蜂窝产生的雷诺数依赖尾流湍流
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-05-31 DOI: 10.1080/14685248.2021.1932944
L. Thijs, R. Dellaert, S. Tajfirooz, J. Zeegers, J. Kuerten
ABSTRACT We present an experimental and numerical study of the flow downstream of honeycomb flow straighteners for a range of Reynolds numbers, covering both laminar and turbulent flow inside the honeycomb cells. We carried out experiments with planar particle image velocimetry (PIV) in a wind tunnel and performed numerical simulations to perform an in-depth investigation of the three-dimensional flow field. The individual channel profiles downstream of the honeycomb gradually develop into one uniform velocity profile. This development corresponds with an increase in the velocity fluctuations which reach a maximum and then start to decay. The position and magnitude of the turbulence intensity peak depend on the Reynolds number. By means of the turbulence kinetic energy (TKE) budget it is shown that the production of TKE is dominated by the shear layers corresponding to the honeycomb walls. The near-field and far-field decay of the turbulence intensity can be described by power laws where we used the position where the production term of the TKE reaches its maximum as the virtual origin.
在一定雷诺数范围内,我们对蜂窝流动矫直器的下游流动进行了实验和数值研究,包括蜂窝单元内的层流和湍流流动。利用平面粒子图像测速技术(PIV)在风洞中进行了实验,并进行了数值模拟,对三维流场进行了深入的研究。蜂窝下游的单个通道剖面逐渐发展成一个均匀的速度剖面。这种发展与速度波动的增加相对应,速度波动达到最大值,然后开始衰减。湍流强度峰的位置和大小取决于雷诺数。通过湍流动能(TKE)的计算表明,TKE的产生主要是由蜂窝壁面对应的剪切层主导的。湍流强度的近场和远场衰减可以用幂律来描述,其中我们使用TKE产生项达到最大值的位置作为虚拟原点。
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引用次数: 3
Estimation of characteristic vortex structures in complex flow 复杂流中特征涡结构的估计
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-05-28 DOI: 10.1080/14685248.2021.1932939
K. Chaudhury, Chandranath Banerjee, Swapnil Urankar
ABSTRACT We present a systematic approach to extract the characteristic vortex region that contains the essential features of a complex flow field. The process involves the analysis of the complex eigenvalues of the velocity gradient tensor. In particular, we propose the analysis using the joint and marginal probability distributions of the complex eigenvalues of the velocity gradient tensor that preserves the sufficient swirling strength and the required orbital compactness of the swirling orbits defining the vortex region. We consider three complex flow scenarios for the application and the assessment of the proposed approach: (i) rotating Rayleigh–Benard convection, (ii) turbulent channel flow, (iii) turbulent flow field in a cylindrical cyclonic separator. While problem (i) is considered for the extraction of subsumed cyclonic structure, problems (ii) and (iii) are reminiscent of wall-bounded turbulent flows, relevant for different industrial applications.
摘要:我们提出了一种系统的方法来提取包含复杂流场基本特征的特征涡流区域。该过程涉及对速度梯度张量的复特征值的分析。特别地,我们提出了使用速度梯度张量的复特征值的联合概率分布和边际概率分布的分析,该分析保持了定义涡流区域的涡流轨道的足够的涡流强度和所需的轨道紧凑性。我们考虑了三种复杂的流动场景来应用和评估所提出的方法:(i)旋转瑞利-贝纳德对流,(ii)湍流通道流,(iii)圆柱形旋风分离器中的湍流场。虽然问题(i)被考虑用于提取包含的气旋结构,但问题(ii)和(iii)让人想起了与不同工业应用相关的壁面湍流。
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引用次数: 1
Cluster-based probabilistic structure dynamical model of wind turbine wake 基于聚类的风力机尾流概率结构动力学模型
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-05-19 DOI: 10.1080/14685248.2021.1925125
N. Ali, M. Calaf, R. B. Cal
For complex flow systems like the one of the wind turbine wakes, which include a range of interacting turbulent scales, there is the potential to reduce the high dimensionality of the problem to low-rank approximations. Unsupervised cluster analysis based on the proper orthogonal decomposition is used here to identify the coherent structure and transition dynamics of wind turbine wake. Through the clustering approach, the nonlinear dynamics of the turbine wake is presented in a linear framework. The features of the fluctuating velocity are grouped based on similarity and presented as the centroids of the defining clusters. Determined from probability distribution of the transition, the dynamical system identifies the features of the wakes and the inherent dynamics of the flow.
对于复杂的流动系统,如风力涡轮机尾迹,其中包括一系列相互作用的湍流尺度,有可能将问题的高维数降低到低秩近似。本文采用基于适当正交分解的无监督聚类分析来识别风力机尾迹的相干结构和转捩动力学。通过聚类方法,将涡轮尾迹的非线性动力学表现在线性框架中。根据相似度对波动速度特征进行分组,并表示为定义簇的质心。动力系统根据转捩的概率分布来识别尾迹的特征和流动的内在动力学。
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引用次数: 7
Transition from axisymmetric to three-dimensional turbulence 从轴对称湍流到三维湍流的过渡
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-05-07 DOI: 10.1080/14685248.2021.1918700
Zecong Qin, A. Naso, W. Bos
In purely axisymmetric turbulence sustained by a linear forcing mechanism, a stable, entirely poloidal flow is observed when the toroidal component of the forcing is below a threshold. We investigate using numerical simulations whether this state persists when toroidal variations of the flow are continuously reintroduced and the forcing is purely poloidal. It is shown how the pressure–strain correlation allows the redistribution of the energy towards the toroidal component. A simple statistical model allows to capture the main physical effects on the level of the global energy balance. This model is then used to investigate the stability of the poloidal state for various toroidal-to-poloidal forcing strengths and different degrees of axisymmetry.
在由线性强迫机制维持的纯轴对称湍流中,当强迫的环形分量低于阈值时,观察到稳定的、完全极向的流动。我们使用数值模拟研究了当流量的环形变化被连续重新引入并且强迫是纯极向的时,这种状态是否会持续。它显示了压力-应变相关性如何允许能量向环形组件重新分布。一个简单的统计模型可以捕捉全球能源平衡水平上的主要物理影响。然后,该模型用于研究不同环面-极向强迫强度和不同轴对称度下极向状态的稳定性。
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引用次数: 0
Special issue on rotating turbulence 旋转湍流特刊
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-05-04 DOI: 10.1080/14685248.2021.1899365
Chao Sun
Rotating Turbulence has attracted extensive research efforts over the last decades due to its fundamental interests and relevance to a variety of natural and engineering processes. The present special issue on Rotating Turbulence collects five contributions from renowned researchers to showcase the variety of physical phenomena and recent advances in this exciting area. This Special Issue is opened by a review paper by L. Biferale, who presents an insightful discussion of Rotating Turbulence with varying degrees of complexity and provides a great introduction to the papers on the special issue. Besides, the paper gives thought-provoking future prospects in this area. The paper of G. Boffetta and coworkers reports a study of freely decaying rotating turbulent flows confined in domains with variable heights using laboratory experiments and numerical simulations. The authors show that vertical confinement has important effects on the formation of large-scale columnar vortices and in particular delays the development of the cyclone–anticyclone asymmetry. This effect is observed both in experiments and in numerical simulations which have structural differences in the boundary conditions, demonstrating the robustness of their findings. The paper by Z. Xia, S. Chen and coworker presents a numerical investigation of the hysteresis behaviour in a spanwise rotating plane Couette flow. By performing two groups of direct numerical simulations where Ro varies in steps along two opposite directions, they demonstrate the existence of hysteresis behaviour in the large-scale realisations at the highest Reynolds number considered, which is also manifested in the turbulent statistics. The paper of R. P. J. Kunnen presents an overview of our current knowledge of the geostrophic regime of turbulent rotating Rayleigh–Bénard convection. The phase diagram of the geostrophic regime of rotating convection is described in detail, with a discussion of the subranges characterised by different flow structures and heat transfer scaling. Complications in the laboratory studies of geostrophic convection are discussed, such as domain size, effects of centrifugal buoyancy, confinement and wall modes, non-Oberbeck–Boussinesq effects and inertial wave resonance. In the paper by S. Horn and J. M. Aurnou, the effects of centrifugal buoyancy on the formation of tornado-like vortices are studied computationally based on the Coriolis-centrifugal convection system. They show that centrifugal buoyancy is relevant for naturally occurring tornadoes and a rich variety of tornado morphologies are produced in the quasi-cyclostrophic regime of Coriolis-centrifugal convection. The Editorial Board thanks the authors for their contributions to the special issue and hopes that this special issue will stimulate further progress and interest in the area.
在过去的几十年里,由于旋转湍流的基本利益和与各种自然和工程过程的相关性,它吸引了广泛的研究努力。本期关于旋转湍流的特刊收集了来自知名研究人员的五篇文章,以展示这个令人兴奋的领域的各种物理现象和最新进展。本特刊由L. Biferale的一篇综述论文开篇,他对不同复杂程度的旋转湍流进行了深刻的讨论,并对特刊上的论文进行了很好的介绍。并对该领域的发展前景进行了展望。G. Boffetta及其同事的论文报告了一项使用实验室实验和数值模拟的研究,该研究限制在可变高度域中的自由衰减旋转湍流。作者认为,垂直约束对大尺度柱状涡的形成有重要影响,特别是延缓了气旋-反气旋不对称的发展。这种效应在边界条件有结构差异的实验和数值模拟中都观察到了,证明了他们的发现的稳健性。夏忠、陈思和同事的论文对沿展向旋转平面Couette流的滞回特性进行了数值研究。通过进行两组直接数值模拟,其中Ro沿两个相反方向的步长变化,他们证明了在考虑的最高雷诺数的大规模实现中存在滞后行为,这也体现在湍流统计中。R. P. J. Kunnen的论文概述了我们目前对湍流旋转瑞利-巴萨姆德对流地转体制的认识。详细描述了旋转对流地转状态的相图,并讨论了以不同流动结构和传热尺度为特征的子范围。讨论了地转对流实验研究中的复杂问题,如区域大小、离心浮力的影响、约束和壁面模式、非奥伯贝克-布西内斯克效应和惯性波共振。S. Horn和J. M. Aurnou基于科里奥利-离心对流系统,计算研究了离心浮力对类龙卷风涡形成的影响。他们表明,离心浮力与自然发生的龙卷风有关,在科里奥利-离心对流的准旋转状态下产生了丰富多样的龙卷风形态。编辑委员会感谢作者为本期特刊所作的贡献,并希望本期特刊将促进该领域的进一步发展和兴趣。
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引用次数: 0
A study of the influence of coflow on flame dynamics in impinging jet diffusion flames 共流对冲击射流扩散火焰动力学影响的研究
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-04-26 DOI: 10.1080/14685248.2021.1917769
Hongxu Li, Jieyu Jiang, Meng Sun, Yongzhe Yu, Chunjie Sui, Bin Zhang
Non-premixed impinging jet flames with different coflow conditions are performed using PIV technology combined with numerical simulation to investigate flame instability in the vicinity of wall. Results indicate that the increase of coflow velocity results in a more chaotic flow field and higher fuel efficiency, and the increase of coflow temperature leads to ignition advance and the increase of NO concentration. These can be attributed to the coupling effect of Kelvin-Helmholtz instability, convective instability and Rayleigh-Taylor instability. High coflow velocity is more likely to induce Kelvin-Helmholtz instability and convective instability, and the increase of coflow temperature enhances Rayleigh-Taylor instability and convective instability. Due to the impact effect in the vicinity of wall, the flame instability is more likely to be induced at high coflow velocity. Meanwhile, the increase of coflow temperature can inhibit flame wrinkles. The flame dynamics is affected by turbulent mixing, head-on collision, shear and convective behaviors in non-premixed flames.
采用PIV技术和数值模拟相结合的方法,研究了不同共流条件下非预混碰撞射流火焰在壁面附近的不稳定性。结果表明,共流速度的增加导致流场更加混乱,燃油效率提高;共流温度的升高导致点火提前和NO浓度的升高。这可归因于Kelvin-Helmholtz不稳定性、对流不稳定性和Rayleigh-Taylor不稳定性的耦合效应。高的共流速度更容易诱发Kelvin-Helmholtz不稳定性和对流不稳定性,共流温度的升高增强了Rayleigh-Taylor不稳定性和对流不稳定性。在高共流速度下,由于壁面附近的冲击效应,更容易诱发火焰不稳定。同时,提高共流温度可以抑制火焰起皱。在非预混火焰中,湍流混合、正面碰撞、剪切和对流行为影响火焰动力学。
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引用次数: 2
Local dynamic perturbation effects on the scale interactions in wall turbulence 局部动力摄动对壁面湍流尺度相互作用的影响
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-03-04 DOI: 10.1080/14685248.2020.1864388
Z. Tang, Xingyu Ma, N. Jiang, Xiaotong Cui, Xiaobo Zheng
An experimental investigation of near-wall scale interactions in the presence of a deterministic forcing input is presented in this work. The external forcing input was generated by a wall-mounted piezoelectric (PZT) actuator, which directly introduces a dynamic perturbation into the near-wall cycle of turbulent boundary layer flow. The spectra of velocity fluctuations indicated that the fundamental forcing mode can be observed in all the perturbed cases and that the occurrence of high-order harmonics is dependent on the PZT perturbation amplitude. Under the strong forcing input, the fundamental forcing mode is influenced by large-scale structures through a high-degree amplitude modulation (AM) effect. More importantly, the phase-switching process was found for the high-order harmonics and small-scale turbulence, both of which are in phase with the forcing mode in and are switched to be out of phase in . It was demonstrated that the forcing mode rearranges both the harmonics and small-scale turbulence in the near-wall region, as evidenced by the AM effect and phase relationship. In addition, the near-wall scale rearrangements were confirmed by the skewness cross-term distribution.
本文对存在确定性强迫输入的近壁尺度相互作用进行了实验研究。外力输入由壁装压电(PZT)致动器产生,该致动器将动态扰动直接引入湍流边界层的近壁循环。速度波动谱表明,在所有扰动情况下都可以观察到基本强迫模式,并且高次谐波的发生与PZT扰动幅度有关。在强强迫输入下,大尺度结构通过高度调幅(AM)效应影响基本强迫模式。更重要的是,发现了高次谐波和小尺度湍流的相位切换过程,这两种情况都与强迫模式同相,并在强迫模式下切换为异相。AM效应和相位关系证明,强迫模式重新排列了近壁区的谐波和小尺度湍流。此外,偏态交叉项分布也证实了近壁尺度的重排。
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引用次数: 3
Dimension reduced turbulent flow data from deep vector quantisers 深度矢量量化器的降维湍流数据
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-03-01 DOI: 10.1080/14685248.2022.2060508
M. Momenifar, Enmao Diao, V. Tarokh, A. Bragg
Analysing large-scale data from simulations of turbulent flows is memory intensive, requiring significant resources. This major challenge highlights the need for data compression techniques. In this study, we apply a physics-informed Deep Learning technique based on vector quantisation to generate a discrete, low-dimensional representation of data from simulations of three-dimensional turbulent flows. The deep learning framework is composed of convolutional layers and incorporates physical constraints on the flow, such as preserving incompressibility and global statistical characteristics of the velocity gradients. The accuracy of the model is assessed using statistical, comparison-based similarity and physics-based metrics. The training data set is produced from Direct Numerical Simulation of an incompressible, statistically stationary, isotropic turbulent flow. The performance of this lossy data compression scheme is evaluated not only with unseen data from the stationary, isotropic turbulent flow, but also with data from decaying isotropic turbulence, a Taylor–Green vortex flow, and a turbulent channel flow. Defining the compression ratio (CR) as the ratio of original data size to the compressed one, the results show that our model based on vector quantisation can offer CR with a mean square error (MSE) of , and predictions that faithfully reproduce the statistics of the flow, except at the very smallest scales where there is some loss. Compared to the recent study of Glaws. et al. [Deep learning for in situ data compression of large turbulent flow simulations. Phys Rev Fluids. 2020;5(11):114602], which was based on a conventional autoencoder (where compression is performed in a continuous space), our model improves the CR by more than 30%, and reduces the MSE by an order of magnitude. Our compression model is an attractive solution for situations where fast, high quality and low-overhead encoding and decoding of large data are required.
分析湍流模拟的大规模数据需要大量的资源,需要大量的记忆。这一重大挑战凸显了对数据压缩技术的需求。在这项研究中,我们应用了一种基于矢量量化的物理深度学习技术,从三维湍流模拟中生成离散的低维数据表示。深度学习框架由卷积层组成,并结合了对流的物理约束,例如保持速度梯度的不可压缩性和全局统计特性。使用统计、基于比较的相似性和基于物理的度量来评估模型的准确性。训练数据集由不可压缩、统计稳定、各向同性湍流的直接数值模拟产生。这种有损数据压缩方案的性能不仅用来自静止各向同性湍流的看不见的数据进行评估,还用来自衰减各向同性湍流、Taylor–Green涡流和湍流通道流的数据进行了评估。将压缩比(CR)定义为原始数据大小与压缩数据大小的比率,结果表明,我们基于矢量量化的模型可以提供均方误差(MSE)为的CR,以及忠实再现流量统计数据的预测,除非在存在一些损失的最小尺度上。与最近对格拉斯的研究相比。等人[用于大湍流模拟的原位数据压缩的深度学习.Phys Rev Fluids.2020;5(11):114602],该模型基于传统的自动编码器(在连续空间中进行压缩),我们的模型将CR提高了30%以上,并将MSE降低了一个数量级。对于需要对大数据进行快速、高质量和低开销编码和解码的情况,我们的压缩模型是一个有吸引力的解决方案。
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引用次数: 8
期刊
Journal of Turbulence
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