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Tornado-like vortices in the quasi-cyclostrophic regime of Coriolis-centrifugal convection 科里奥利离心对流准涡旋区的类龙卷风涡旋
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-03-01 DOI: 10.1080/14685248.2021.1898624
S. Horn, J. Aurnou
Coriolis-centrifugal convection ( ) in a cylindrical domain constitutes an idealised model of tornadic storms, where the rotating cylinder represents the mesocyclone of a supercell thunderstorm. We present a suite of direct numerical simulations, analysing the influence of centrifugal buoyancy on the formation of tornado-like vortices (TLVs). TLVs are self-consistently generated provided the flow is within the quasi-cyclostrophic (QC) regime in which the dominant dynamical balance is between pressure gradient and centrifugal buoyancy forces. This requires the Froude number to be greater than the radius-to-height aspect ratio, . We show that the TLVs that develop in our simulations share many similar features with realistic tornadoes, such as azimuthal velocity profiles, intensification of the vortex strength, and helicity characteristics. Further, we analyse the influence of the mechanical bottom boundary conditions on the formation of TLVs, finding that a rotating fluid column above a stationary surface does not generate TLVs if centrifugal buoyancy is absent. In contrast, TLVs are generated in the QC regime with any bottom boundary conditions when centrifugal buoyancy is present. Our simulations bring forth insights into natural supercell thunderstorm systems by identifying properties that determine whether a mesocyclone becomes tornadic or remains non-tornadic. For tornadoes to exist, a vertical temperature difference must be present that is capable of driving strong convection. Additionally, our predictions dimensionally imply a critical mesocyclone angular rotation rate of . Taking a typical mesocyclone height of , this translates to for centrifugal buoyancy-dominated, quasi-cyclostrophic tornadogenesis. The formation of the simulated TLVs happens at all heights on the centrifugal buoyancy time scale . This implies a roughly 1 minute, height-invariant formation for natural tornadoes, consistent with recent observational estimates.
圆柱形区域中的科里奥利离心对流()构成了龙卷风的理想化模型,其中旋转的圆柱体代表超级单体雷暴的中气旋。我们提出了一套直接的数值模拟,分析了离心浮力对龙卷风状旋涡(TLV)形成的影响。TLV是自洽产生的,前提是流量在准气旋(QC)范围内,其中主要的动力平衡是在压力梯度和离心浮力之间。这需要弗劳德数大于半径与高度的纵横比。我们表明,在我们的模拟中开发的TLV与现实龙卷风有许多相似的特征,如方位角速度剖面、涡流强度的增强和螺旋度特征。此外,我们分析了机械底部边界条件对TLV形成的影响,发现如果没有离心浮力,静止表面上方的旋转液柱不会产生TLV。相反,当存在离心浮力时,TLV是在具有任何底部边界条件的QC状态下产生的。我们的模拟通过识别决定中气旋是成为龙卷风还是保持非龙卷风的特性,为自然超级单体雷暴系统提供了见解。龙卷风要想存在,就必须存在能够驱动强对流的垂直温差。此外,我们的预测在维度上暗示了临界中气旋角旋转速率为。以典型的中气旋高度为,这意味着离心浮力主导的准气旋龙卷风生成。模拟TLV的形成发生在离心浮力时间尺度上的所有高度。这意味着自然龙卷风的形成时间大约为1分钟,高度不变,与最近的观测估计一致。
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引用次数: 10
Impulse response of turbulent flow in smooth and riblet-walled channels to a sudden velocity increase 光滑沟道和波纹壁沟道湍流对速度突然增加的脉冲响应
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-02-16 DOI: 10.1080/14685248.2021.1885676
S. Pargal, J. Yuan, G. Brereton
ABSTRACT This paper explores the use of a small-span direct numerical simulation for a transient, smooth-wall turbulent channel flow and then applies the small-span simulation to a transient channel flow with riblets. A flow configuration similar to that of S. He and M. Seddighi (J Fluid Mech. 2013;715:60–102) is used to study the impulse response of a half-height channel flow to an abrupt increase in bulk velocity (with a friction Reynolds number increasing from 180 to 418). A minimal domain span sufficient to include the near-wall quasi-streamwise vortices in the ‘healthy turbulence’ region is used. The turbulent flow undergoes reverse transition toward a quasi-laminar state, followed by a retransition phase to the new equilibrium state. On a smooth wall, detailed comparisons with a full-span case show that the small-span test case captures satisfactorily the essential dynamics during the entire transition process, although it yields a slight delay in recovery to the new equilibrium. This difference is attributed to a slower streak transient growth due to an underestimation of near-wall spanwise fluctuations. This underestimation is associated with the missing large attached eddies that are not contained in the small span of the simulation domain. These comparisons justify the use of small-span simulations for identifying the main flow physics in a non-equilibrium accelerating wall turbulence. The application to the riblet flow shows that riblets do not fundamentally affect the flow dynamics, but delay the retransition as a result of significantly milder streak meandering. The streak-stabilisation effect of riblets is still active in a strongly accelerating turbulence and tends to prolong the flow recovery.
摘要本文探讨了瞬态光滑壁湍流通道流动的小跨度直接数值模拟方法,并将其应用于带纹的瞬态通道流动。采用类似S. He和M. Seddighi (J Fluid Mech. 2013; 715:60-102)的流动构型研究了半高通道流动对体速度突然增加(摩擦雷诺数从180增加到418)的脉冲响应。在“健康湍流”区域中,使用了足以包含近壁面准流向涡的最小域跨度。紊流经过向准层流状态的反向过渡,然后再过渡到新的平衡状态。在光滑的墙壁上,与全跨度案例的详细比较表明,小跨度测试用例在整个过渡过程中令人满意地捕获了基本动态,尽管它在恢复到新的平衡方面产生了轻微的延迟。这种差异是由于对近壁展向波动的低估导致条纹瞬态增长较慢。这种低估与缺少大的附加涡流有关,这些涡流不包含在模拟域的小范围内。这些比较证明了使用小跨度模拟来识别非平衡加速壁面湍流中的主流物理。对纹状流的应用表明,纹状流并不从根本上影响流动动力学,但由于纹状流的弯曲明显减弱,从而延迟了再转变。在强加速湍流中,纹条的稳定作用仍然有效,并有延长流动恢复的趋势。
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引用次数: 2
Numerical investigation on ultra-high-lift low-pressure turbine cascade aerodynamics at low Reynolds numbers using transition-based turbulence models 基于过渡的湍流模型对低雷诺数下超高升力低压涡轮叶栅气动特性的数值研究
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-02-01 DOI: 10.1080/14685248.2020.1849712
Xiaole Wang, B. Cui, Zuoli Xiao
ABSTRACT The performance of ultra-high-lift (UHL) low-pressure turbine (LPT) is subject to complex flow phenomena (e.g. separation, transition and reattachment) which require advanced modelling for accurate numerical predictions. The feasibility and fidelity of three widely used transition-based turbulence models are evaluated in the Reynolds-Averaged Navier-Stokes (RANS) prediction of low-Reynolds number flows in linear UHL LPT cascade (T106C). All three transition models prove to capture the tendency that the size of separation bubble decreases with the increase of Reynolds number or inlet turbulence intensity. It turns out that intermittency factor-transition momentum thickness Reynolds number based shear stress transport turbulence model is the most accurate among the three models, expect for the clean inlet case at an isentropic outlet Reynolds number of . It is suggested that different viscosity ratios should be prescribed at the inlet for various models to mimic the effect of turbulence intensities precisely. In order to take into account the periodic wakes in computation, a moving cylindrical bar is added to the cascade inlet. The assessment of the capability of three models in predicting unsteady wake induced transition is carried out for selected Reynolds numbers. Some practical suggestions are given for the use of transition models based on RANS equations in simulation of the ultra-high-lift LPT cascade flows at low Reynolds numbers.
摘要超高升程(UHL)低压涡轮机(LPT)的性能受到复杂流动现象(如分离、过渡和再附着)的影响,需要先进的建模才能进行准确的数值预测。在雷诺平均Navier-Stokes(RANS)预测超高压低雷诺数线性叶栅(T106C)中,评估了三种广泛使用的基于过渡的湍流模型的可行性和保真度。三个过渡模型都证明了分离气泡尺寸随雷诺数或入口湍流强度的增加而减小的趋势。结果表明,基于雷诺数的剪切应力输运湍流模型是三种模型中最准确的,除了等熵出口雷诺数为的清洁入口情况。建议在各种模型的入口处规定不同的粘度比,以精确模拟湍流强度的影响。为了在计算中考虑周期尾流,在叶栅入口处增加了一个移动的圆柱杆。针对选定的雷诺数,对三个模型预测非定常尾流诱导过渡的能力进行了评估。对基于RANS方程的过渡模型在低雷诺数超高升程LPT叶栅流动模拟中的应用提出了一些实用建议。
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引用次数: 5
The geostrophic regime of rapidly rotating turbulent convection 快速旋转湍流对流的地转状态
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2021-01-26 DOI: 10.1080/14685248.2021.1876877
R. Kunnen
Rotating Rayleigh–Bénard convection is a simple model system used to study the interplay of buoyant forcing and rotation. Many recent studies have focused on the geostrophic regime of turbulent rotating convection where the principal balance of forces is between the Coriolis force and the pressure gradient. This regime is believed to be representative of conditions in geophysical and astrophysical flows. We hope to be able to extrapolate findings from laboratory experiments and numerical simulations towards these large-scale natural flows. In this paper I sketch the phase diagram of the geostrophic regime of rotating convection, put experimental and numerical studies in their place in these diagrams and discuss the partitioning into subranges characterised by different flow structures and heat transfer scaling. I also discuss some complications faced by experimentalists, such as constraints on the dimensions of the convection cell, wall modes near the sidewall and centrifugal buoyancy.
旋转Rayleigh–Bénard对流是一个简单的模型系统,用于研究浮力和旋转的相互作用。最近的许多研究都集中在湍流旋转对流的地转状态上,其中力的主要平衡在科里奥利力和压力梯度之间。这种情况被认为是地球物理和天体物理流动条件的代表。我们希望能够从实验室实验和数值模拟中推断出这些大规模自然流动的结果。在本文中,我绘制了旋转对流地转区的相图,将实验和数值研究放在这些图中,并讨论了以不同的流动结构和传热标度为特征的子范围的划分。我还讨论了实验者面临的一些复杂问题,如对流池尺寸的限制、侧壁附近的壁模式和离心浮力。
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引用次数: 29
Numerical investigation and triple-parameters correlations development on the dynamic characteristics of a turbulent offset jet 湍流偏置射流动力学特性的数值研究和三参数关联发展
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2020-12-29 DOI: 10.1080/14685248.2020.1863416
M. Ajmi, N. Hnaien, Saloua Marzouk, Lioua Kolsi, Kaouther Ghachem, H. B. Aissia
ABSTRACT The present numerical study aims to numerically investigate the dynamic and turbulent characteristics of a two-dimensional and turbulent offset jet. Three different parameters were investigated: The Reynolds numbers (Re) which was varied from 10000 to 30000, wall inclination angle (α) that was from −20° to +20° and finally the offset ratio (OR) which extends from 3.25–13. Ansys Fluent was numerical CFD solver used in this present investigation. The simultaneous effects of the OR, Re and α were investigated in details. The velocity and pressure contours showed that these three parameters do not contribute equally in the development of such a flow. Also, the turbulent characteristics, such as the turbulence intensities and energies depicted how each parameter influences, separately, the turbulent flow production. Furthermore, different of tripled parameters correlations were developed. These correlations may be of help to more understand certain offset jet flow features more accurately and to predict their exact values.
摘要本数值研究旨在对二维湍流偏置射流的动力学和湍流特性进行数值研究。研究了三个不同的参数:雷诺数(Re)在10000到30000之间变化,壁倾角(α)在−20°到+20°之间变化,最后偏移比(OR)在3.25到13之间变化。Ansys Fluent是本研究中使用的CFD数值求解器。详细研究了OR、Re和α的同时作用。速度和压力等值线表明,这三个参数对这种流动的发展没有同等的贡献。此外,湍流特性,如湍流强度和能量,描述了每个参数如何单独影响湍流的产生。此外,还建立了不同的三倍参数相关性。这些相关性可能有助于更准确地理解某些偏移射流特征,并预测其确切值。
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引用次数: 2
Assessment of turbulence models for single phase CFD computations of a liquid-liquid hydrocyclone using OpenFOAM 使用OpenFOAM评估液-液水力旋流器单相CFD计算的湍流模型
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2020-12-29 DOI: 10.1080/14685248.2020.1846050
Rodrigo Petrone dos Anjos, Ricardo de Andrade Medronho, Tânia Suaiden Klein
ABSTRACT Hydrocyclones are widely used in industry and CFD has been used to compute them. Reynolds stress turbulence models (RSM), which are computationally costly and oftentimes hard to converge, are often recommended in these computations. The present work has selected a liquid-liquid separation hydrocyclone for which single-phase experimental tangential and axial velocity profiles are available. CFD has been employed to test simpler turbulence models than the RSM and results have been compared with experimental data. The turbulence models assessed in the present work were: standard k-ε, standard k-ε with a curvature correction term, RNG k-ε, realizable k-ε, k-ω, SST, a two-time-scale linear eddy viscosity model, nonlinear quadratic and cubic k-ε eddy viscosity models and the Gibson and Launder and LRR Reynolds stress models. Computations have been carried out with OpenFOAM 2.2.2. Results using the Gibson and Launder turbulence model have been compared to some obtained with Ansys Fluent and these were in agreement. Results have shown that all turbulence models, apart from the RSM, returned basically the same tangential velocity profiles as the standard model. All turbulence models have failed in predicting axial velocity. Assessment of the Reynolds stresses has indicated that the internal flow field in hydrocyclones might be shear dominant and that the Reynolds shear stress component is the most relevant to correctly predict tangential velocity. Geometric proportions of hydrocyclones may affect significantly the intensity of rotational and streamline curvature effects. Two-equation eddy-viscosity models are likely to be able to attend such condition, since appropriate levels of eddy viscosity are predicted at free and forced vortexes regions, however further investigation is still needed.
水力旋流器在工业上有着广泛的应用,CFD已被用于水力旋流器的计算。雷诺应力湍流模型(RSM)计算成本高,往往难以收敛,在这些计算中经常被推荐使用。本工作选择了一种液液分离水力旋流器,它的单相实验切向和轴向速度分布是可用的。用CFD测试了比RSM更简单的湍流模型,并将结果与实验数据进行了比较。本文评估的湍流模型有:标准k-ε、带曲率修正项的标准k-ε、RNG k-ε、可实现k-ε、k-ω、SST、两时间尺度线性涡粘度模型、非线性二次和三次k-ε涡粘度模型以及Gibson和Launder和LRR Reynolds应力模型。使用OpenFOAM 2.2.2进行计算。用Gibson和Launder湍流模型得到的结果与Ansys Fluent得到的结果相比较,两者是一致的。结果表明,除RSM模型外,所有湍流模型返回的切向速度曲线与标准模型基本相同。所有湍流模型都无法预测轴向速度。对旋流器内部流场的雷诺应力评估表明,旋流器内部流场可能以剪切为主,而雷诺剪切应力分量与正确预测切向速度最相关。旋流器的几何比例会显著影响旋流器的旋转和流线曲率效应的强度。由于在自由涡区和受迫涡区预测了适当的涡黏度水平,双方程涡黏度模型可能能够处理这种情况,但仍需要进一步的研究。
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引用次数: 1
Hysteresis behaviour in spanwise rotating plane Couette flow at Re w = 2600 Re w=2600时展向旋转平面Couette流的磁滞行为
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2020-12-09 DOI: 10.1080/14685248.2020.1856859
Yuhan Huang, Zhenhua Xia, Shiyi Chen
Hysteresis behaviour was reported in spanwise rotating plane Couette flow (RPCF) at Reynolds number with varying rotation number in a recent work (Huang et al. Phys. Rev. Fluids 2019;4:052401(R)). Here, is half of the velocity difference between two walls, h is half of the channel width, ν is the kinematic viscosity and is the constant angular velocity in the spanwise direction. In this paper, we perform two groups of direct numerical simulations at where Ro varies in steps along two opposite directions to investigate the hysteresis behaviour in RPCF at a relatively higher Reynolds number. It is found that when Reynolds number increases to 2600, the hysteresis of flow structures still exists in RPCF, but the span of the hysteresis loop shrinks from to . Turbulent statistics, such as the friction Reynolds number, turbulent kinetic energy and mean velocity gradient at the centreline, all exhibit similar hysteresis behaviours.
在最近的一项研究中,研究人员报道了沿展向旋转平面库埃特流(RPCF)在雷诺数变化时的滞回行为。理论物理。流体力学学报(英文版);2019;4:052 - 401(R)。这里,是两个壁面之间速度差的一半,h是通道宽度的一半,ν是运动粘度,是沿展向的恒定角速度。在本文中,我们进行了两组直接数值模拟,其中Ro沿两个相反方向的步长变化,以研究相对较高雷诺数下RPCF的滞后行为。研究发现,当雷诺数增加到2600时,RPCF中流动结构的迟滞仍然存在,但迟滞回路的跨度从减小到。湍流统计数据,如摩擦雷诺数、湍流动能和中线的平均速度梯度,都表现出类似的滞后行为。
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引用次数: 0
RANS Model development on temperature variance in conjugate heat transfer 共轭传热中温度变化的RANS模型的发展
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2020-12-02 DOI: 10.1080/14685248.2020.1860214
Gao Yang, H. Iacovides, T. Craft, D. Apsley
In this study, a RANS model of turbulent conjugate heat transfer has been developed, which is applicable across a range of different combination of fluid and solid thermal properties. This is achieved by focusing on the transport equations for the temperature variance and its dissipation rate across the solid walls which bound the flow region. In this investigation we make use of a wider range of DNS data reported by other researchers, to advance our understanding of the processes involved and to revise and extend the capabilities of the model of Craft et al [12] including a more physical fluid-solid interface condition on the dissipation of thermal fluctuations and a dependence of model coefficients on Prandtl number. The resulting model is shown to successfully reproduce the penetration of thermal fluctuations into solid regions, and their subsequent decay across the solid, for a wide range of fluid to solid thermal property ratios, and Prandtl numbers, thereby bringing a step change to RANS capabilities in turbulent conjugate heat transfer analysis.
本研究建立了紊流共轭传热的RANS模型,该模型适用于一系列不同的流体和固体热性质组合。这是通过关注温度方差的输运方程及其在束缚流动区域的固体壁上的耗散率来实现的。在本研究中,我们利用其他研究人员报告的更广泛的DNS数据,以提高我们对所涉及过程的理解,并修改和扩展Craft等人的模型的能力[0],包括更物理的流固界面条件,热波动的耗散和模型系数对普朗特数的依赖。结果表明,该模型成功地再现了热波动对固体区域的渗透,以及它们随后在固体中的衰减,适用于大范围的流体与固体热性能比和普朗特尔数,从而使RANS在湍流共轭传热分析中的能力发生了阶跃变化。
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引用次数: 1
Cyclone–anticyclone asymmetry in rotating thin fluid layers 旋转薄流体层中的气旋-反气旋不对称性
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2020-12-02 DOI: 10.1080/14685248.2020.1855352
G. Boffetta, Francesco Toselli, M. Manfrin, S. Musacchio
We report of a series of laboratory experiments and numerical simulations of freely decaying rotating turbulent flows confined in domains with variable height. We show that the vertical confinement has important effects on the formation of large-scale columnar vortices, the hallmark of rotating turbulence, and in particular delays the development of the cyclone–anticyclone asymmetry. We compare the experimental and numerical results face-to-face, showing the robustness of the results.
我们报告了一系列的实验室实验和数值模拟的自由衰减旋转湍流限制在可变高度的区域。我们发现垂直约束对大尺度柱状涡的形成有重要影响,这是旋转湍流的标志,特别是延迟了气旋-反气旋不对称的发展。我们将实验结果与数值结果进行了面对面的比较,证明了结果的稳健性。
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引用次数: 4
Experimental investigation of the influence of Reynolds number and buoyancy on the flow development of a plane jet in the transitional regime 雷诺数和浮力对过渡区平面射流流动发展影响的实验研究
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2020-12-02 DOI: 10.1080/14685248.2020.1849710
P. Suresh, T. Sundararajan, K. Srinivasan, Sarit K. Das
Heated horizontal plane jets find wide applications in engineering appliances such as air curtains and discharge of industrial effluents. In the present study, experimental investigations are conducted on a heated horizontal plane jet with the Reynolds numbers in the transitional regime, using a hotwire anemometer. In the far to very far-field (20 < x/d < 100) centreline velocity decay and jet spread increases faster with the decrease of Reynolds number. This is because, with the increase of Reynolds number, the turbulent kinetic energy is distributed on a broadband of scales. As a result, larger scales, which are responsible for increased entrainment, get weaker. The shifting of the centre plane generally occurs in the far region for low Reynolds number jets. A comparison with the result of an isothermal jet at similar Reynolds numbers from the literature at identical conditions shows that the turbulence intensity is decreased due to heating. Centreline velocity decays slowly and half-width increases marginally for a heated jet when compared with an isothermal jet. The effect of heating is prominent for low Re jets. Spectral development shows a delayed transition due to heating. Probability density function plots reveal lack of equilibrium and presence of large-scale eddies in the flow field.
加热水平面射流在工程设备中有着广泛的应用,如空气幕和工业废水排放。在本研究中,使用热线风速计对雷诺数处于过渡区的加热水平面射流进行了实验研究。在遥远的领域(20 < x/d < 100)随着雷诺数的减小,中心线速度衰减和射流扩散增加得更快。这是因为,随着雷诺数的增加,湍流动能在宽带尺度上分布。因此,导致夹带增加的较大规模变得较弱。对于低雷诺数射流,中心平面的偏移通常发生在较远的区域。与文献中相同条件下雷诺数相似的等温射流结果的比较表明,由于加热,湍流强度降低。与等温射流相比,加热射流的中心线速度衰减缓慢,半宽略有增加。对于低Re射流,加热的影响是显著的。光谱发展显示由于加热而延迟转变。概率密度函数图揭示了流场中缺乏平衡和存在大规模涡流。
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引用次数: 0
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Journal of Turbulence
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