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Mixing as a correlated aggregation process 作为相关聚合过程的混合
IF 3.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-08-27 DOI: 10.1017/jfm.2024.537
J. Heyman, E. Villermaux, P. Davy, T. Le Borgne
Mixing describes the process by which solutes evolve from an initial heterogeneous state to uniformity under the stirring action of a fluid flow. Fluid stretching forms thin scalar lamellae that coalesce due to molecular diffusion. Owing to the linearity of the advection–diffusion equation, coalescence can be envisioned as an aggregation process. Here, we demonstrate that in smooth two-dimensional chaotic flows, mixing obeys a correlated aggregation process, where the spatial distribution of the number of lamellae in aggregates is highly correlated with their elongation, and is set by the fractal properties of the advected material lines. We show that the presence of correlations makes mixing less efficient than a completely random aggregation process because lamellae with similar elongations and scalar levels tend to remain isolated from each other. We show that correlated aggregation is uniquely determined by a single exponent that quantifies the effective number of random aggregation events. These findings expand aggregation theories to a larger class of systems, which have relevance to various fundamental and applied mixing problems.
混合描述了在流体流动的搅拌作用下,溶质从最初的异质状态演变为均匀状态的过程。流体拉伸形成薄薄的标量薄片,这些薄片由于分子扩散而凝聚在一起。由于平流-扩散方程的线性关系,凝聚可以看作是一个聚集过程。在这里,我们证明了在平滑的二维混沌流中,混合遵从一个相关的聚集过程,聚集体中薄片数量的空间分布与它们的伸长高度相关,并且由平流材料线的分形特性决定。我们的研究表明,相关性的存在使得混合的效率低于完全随机的聚集过程,因为具有相似伸长率和标量水平的薄片往往会相互隔离。我们的研究表明,相关聚集是由单一指数唯一决定的,该指数量化了随机聚集事件的有效数量。这些发现将聚集理论扩展到了更大的系统类别,与各种基础和应用混合问题息息相关。
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引用次数: 0
Direct numerical simulation of 45° oblique flow past surface-mounted square cylinder 45° 斜向流经表面安装方形圆筒的直接数值模拟
IF 3.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-08-27 DOI: 10.1017/jfm.2024.554
Dung Viet Duong, Luc Van Nguyen, Duc Van Nguyen, Truong Cong Dinh, Lavi Rizki Zuhal, Long Ich Ngo
Comprehensive coherent structures around a surface-mounted low aspect ratio square cylinder in uniform flow with an oblique angle of $45^{circ }$ were investigated for cylinder-width-based Reynolds numbers of 3000 and 10 000 by direct numerical simulation based on a topology-confined mesh refinement framework. High-resolution simulations and the critical-point concept were scrutinized to reveal for the first time the reasonable and compatible topologies of flow separation and complete near-wall structures, due to their extensive impact on various engineering applications. Large-scale horseshoe vortices are observed at two notable foci in the viscous sublayer. Within this layer, a wall-parallel jet is formed by downflow intruding into the bottom surface at the half-saddle point, then deflecting in the upstream direction and finally penetrating the bottom surface until the half-saddle point. A pair of conical vortices on the cylinder's top surface switch themselves on two sides of the square cylinder, where the switching frequency is identical with that of the sway of the side shear layer. The undulation of the Kelvin–Helmholtz instability is identified in the instantaneous development of a conical vortex and side shear layer, where the scaling of the ratio of the Kelvin–Helmholtz and von Kármán frequencies follows the power-law relation obtained by Lander et al. (J. Fluid Mech., vol. 849, 2018, pp. 1096–1119). Large-scale arch-shaped vortex is often detected in the intermediate wake region of a square cylinder, involving two interconnected portions, such as the leg portion separated from leeward surfaces and head portion rolled up from the top surface. The leg portion of the arch-shaped vortex was rooted by two foci near the bottom-surface plane.
通过基于拓扑约束网格细化框架的直接数值模拟,研究了在斜角为 $45^{circ }$ 的均匀流中,基于圆柱体宽度的雷诺数为 3000 和 10 000 时,表面安装的低纵横比方形圆柱体周围的综合相干结构。由于高分辨率模拟和临界点概念对各种工程应用的广泛影响,研究首次揭示了流体分离和完整近壁结构的合理兼容拓扑结构。在粘性子层的两个显著焦点处观察到了大尺度马蹄涡。在这一层中,下流在半鞍点侵入底面,然后向上游方向偏转,最后穿透底面直至半鞍点,形成了与壁面平行的射流。圆柱体顶面的一对锥形涡流在方形圆柱体的两侧切换,切换频率与侧剪切层的摇摆频率相同。开尔文-赫尔姆霍兹不稳定性的起伏在锥形涡旋和侧剪切层的瞬时发展中得以确定,其中开尔文-赫尔姆霍兹频率和冯-卡尔曼频率的比例关系遵循 Lander 等人获得的幂律关系(《流体力学》,第 849 卷,2018 年,第 1096-1119 页)。在方形圆柱体的中间尾流区域经常检测到大尺度拱形涡旋,涉及两个相互连接的部分,如与背风面分离的腿部和从顶面卷起的头部。拱形涡旋的腿部由靠近底面平面的两个焦点构成。
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引用次数: 0
Emergence of lobed wakes during the sedimentation of spheres in viscoelastic fluids 粘弹性流体中球体沉积过程中出现的叶状漩涡
IF 3.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-08-27 DOI: 10.1017/jfm.2024.459
Stylianos Varchanis, Eliane Younes, Simon J. Haward, Amy Q. Shen
The motion of rigid particles in complex fluids is ubiquitous in natural and industrial processes. The most popular toy model for understanding the physics of such systems is the settling of a solid sphere in a viscoelastic fluid. There is general agreement that an elastic wake develops downstream of the sphere, causing the breakage of fore-and-aft symmetry, while the flow remains axisymmetric, independent of fluid viscoelasticity and flow conditions. Using a continuum mechanics model, we reveal that axisymmetry holds only for weak viscoelastic flows. Beyond a critical value of the settling velocity, steady, non-axisymmetric disturbances develop peripherally of the rear pole of the sphere, giving rise to a four-lobed fingering instability. The transition from axisymmetric to non-axisymmetric flow fields is characterized by a regular bifurcation and depends solely on the interplay between shear and extensional properties of the viscoelastic fluid under different flow regimes. At higher settling velocities, each lobe tip is split into two new lobes, resembling fractal fingering in interfacial flows. For the first time, we capture an elastic fingering instability under steady-state conditions, and provide the missing information for understanding and predicting such instabilities in the response of viscoelastic fluids and soft media.
刚性粒子在复杂流体中的运动在自然和工业过程中无处不在。为了解此类系统的物理原理,最常用的玩具模型是固体球体在粘弹性流体中的沉降。人们普遍认为,球体下游会产生弹性尾流,导致前后对称性被破坏,而流体仍保持轴对称,与流体粘弹性和流动条件无关。利用连续介质力学模型,我们发现轴对称只适用于弱粘弹性流动。当沉降速度超过临界值时,球体后极外围会出现稳定的非轴对称扰动,从而引发四叶指状不稳定性。从轴对称流场到非轴对称流场的过渡具有规则分岔的特征,完全取决于粘弹性流体在不同流动状态下的剪切和延伸特性之间的相互作用。在较高的沉降速度下,每个叶尖分裂成两个新叶,类似于界面流中的分形指状。我们首次捕捉到了稳态条件下的弹性指状不稳定性,为理解和预测粘弹性流体和软介质响应中的此类不稳定性提供了缺失的信息。
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引用次数: 0
Non-local gravity wave turbulence in presence of condensate 存在凝结剂的非局部重力波湍流
IF 3.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-08-27 DOI: 10.1017/jfm.2024.423
Alexander O. Korotkevich, Sergey V. Nazarenko, Yulin Pan, Jalal Shatah
The $k^{-23/6}$ wave action spectrum with an inverse cascade is one of the fundamental Kolmogorov–Zakharov solutions for gravity wave turbulence, which is part of the citation for the Dirac Medal in 2003. Instead of confirming this solution, however, several existing simulations and experiments suggest a spectrum of $k^{-3}$ in set-ups corresponding to the inverse cascade. We provide a theoretical explanation for the latter, considering the condensate that naturally forms in finite domains of experiments/simulations. Our new theory hinges on: (1) derivation of a spectral diffusion equation when non-local interactions with the condensate become dominant, for the first time systematically formulated for quartet-interaction systems; and (2) careful analysis of the asymptotics of interaction coefficient with a remarkable cancellation of all leading-order terms.
具有反级联的 $k^{-23/6}$ 波作用谱是重力波湍流的基本科尔莫戈罗夫-扎哈罗夫解法之一,也是 2003 年狄拉克奖章的引文之一。然而,现有的一些模拟和实验并没有证实这一解决方案,反而表明在与反级联相对应的设置中存在 $k^{-3}$ 的频谱。考虑到在实验/模拟的有限域中自然形成的凝聚态,我们为后者提供了理论解释。我们的新理论取决于(1) 当与凝结物的非局部相互作用成为主导时,推导出一个谱扩散方程,这是第一次系统地为四元相互作用系统制定这个方程;(2) 仔细分析相互作用系数的渐近线,显著取消所有前导阶项。
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引用次数: 0
On the coupling instability of a gas jet impinging on a liquid film 关于撞击液膜的气体射流的耦合不稳定性
IF 3.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-08-27 DOI: 10.1017/jfm.2024.553
David Barreiro-Villaverde, Anne Gosset, Marcos Lema, Miguel A. Mendez
We investigate the dynamics of a gas jet impinging perpendicular to a thin liquid film dragged by a rising vertical substrate. This configuration is relevant to the jet-wiping process in hot-dip galvanization and it is unstable. Previous studies analysed the dynamics of the instability in the case of liquids with low Kapitza numbers (highly viscous liquids), more amenable to experimental and numerical investigations. This work extends the previous investigations by focusing on the wiping at much higher Kapitza numbers, which are more relevant to the galvanizing process. The simulations are carried out by combining volume of fluid and large-eddy simulations, and the dynamics of the gas–liquid interaction is analysed using extended multiscale proper orthogonal decomposition. The simulations allowed for analysing the jet-wiping instability in new flow conditions. Despite the largely different conditions, the results show that the interaction between the gas jet and the liquid film is qualitatively similar, featuring two-dimensional waves in the liquid correlated with oscillations and deflections of the gas jet in all cases. The wave characteristics (e.g. frequency and propagation speed) scale remarkably well using the Shkadov-like scaling based on the liquid, suggesting a dominant role of the liquid film in the coupling, and potentially enabling extrapolation of the results to a broader range of wiping conditions. Finally, we use the numerical results to discuss the limitations of liquid-film models, which constitute currently the only possible approach to study the jet-wiping process in industrial conditions.
我们研究了垂直于被上升的垂直基底拖动的薄液膜的气体射流的动力学。这种构造与热镀锌中的喷射擦拭过程有关,而且不稳定。之前的研究分析了 Kapitza 数较低的液体(高粘度液体)的不稳定性动态,更适合进行实验和数值研究。这项工作扩展了之前的研究,重点关注 Kapitza 数高得多的擦拭情况,这与镀锌工艺更为相关。模拟结合了流体体积模拟和大涡流模拟,并使用扩展多尺度适当正交分解分析了气液相互作用的动力学。模拟分析了新流动条件下的喷流擦拭不稳定性。尽管条件大不相同,但结果表明气体射流和液膜之间的相互作用在本质上是相似的,在所有情况下,液体中的二维波与气体射流的振荡和偏转相关。波的特性(如频率和传播速度)使用基于液体的类似于什卡托夫(Shkadov)的缩放比例非常好,这表明液膜在耦合中起着主导作用,并有可能将结果推广到更广泛的擦拭条件中。最后,我们利用数值结果讨论了液膜模型的局限性,该模型是目前研究工业条件下喷射擦拭过程的唯一可行方法。
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引用次数: 0
Thin-film flow due to an asymmetric distribution of surface tension and applications to surfactant deposition 表面张力不对称分布导致的薄膜流动及其在表面活性剂沉积中的应用
IF 3.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-08-27 DOI: 10.1017/jfm.2024.501
Jun Eshima, Luc Deike, Howard A. Stone
Thin-film equations are utilised in many different areas of fluid dynamics when there exists a direction in which the aspect ratio can be considered small. We consider thin free films with Marangoni effects in the extensional flow regime, where velocity gradients occur predominantly along the film. In practice, because of the local deposition of surfactants or input of energy, asymmetric distributions of surfactants or surface tension more generally, are possible. Such examples include the surface of bubbles and the rupture of thin films. In this study, we consider the asymmetric thin-film equations for extensional flow with Marangoni effects. Concentrating on the case of small Reynolds number $ Re $ , we study the deposition of insoluble surfactants on one side of a liquid sheet otherwise at rest and the resulting thinning and rupture of the sheet. The analogous problem with a uniformly thinning liquid sheet is also considered. In addition, the centreline deformation is discussed. In particular, we show analytically that if the surface tension isotherm $sigma = sigma (varGamma )$ is nonlinear (surface tension $sigma$ varies with surfactant concentration $varGamma$ ), then accounting for top–bottom asymmetry leads to slower (faster) thinning and pinching if $sigma = sigma (varGamma )$ is convex (concave). The analytical progress reported in this paper allows us to discuss the production of satellite drops from rupture via Marangoni effects, which, if relevant to surface bubbles, would be an aerosol production mechanism that is distinct from jet drops and film drops.
在流体动力学的许多不同领域,当存在一个纵横比很小的方向时,薄膜方程都会被使用。我们考虑的是在延伸流动状态下具有马兰戈尼效应的自由薄膜,在这种状态下,速度梯度主要沿着薄膜发生。实际上,由于表面活性剂的局部沉积或能量输入,表面活性剂或表面张力的非对称分布是可能的。例如气泡表面和薄膜破裂。在本研究中,我们考虑了具有马兰戈尼效应的伸展流动的非对称薄膜方程。我们集中研究了小雷诺数 $ Re $ 的情况,研究了不溶性表面活性剂在静止液膜一侧的沉积以及由此导致的液膜变薄和破裂。我们还考虑了均匀变薄液面的类似问题。此外,我们还讨论了中心线变形问题。特别是,我们通过分析表明,如果表面张力等温线 $sigma = sigma (varGamma )$ 是非线性的(表面张力 $sigma$ 随表面活性剂浓度 $varGamma$ 变化而变化),那么如果 $sigma = sigma (varGamma )$ 是凸形(凹形)的,则考虑到上下不对称会导致变薄和挤压变慢(变快)。本文所报告的分析进展使我们能够讨论通过马兰戈尼效应从破裂处产生卫星气滴的问题,如果这与表面气泡有关,那么这将是一种有别于喷流气滴和薄膜气滴的气溶胶产生机制。
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引用次数: 0
Dewetting of a corner film wrapping a wall-mounted cylinder 壁挂式圆筒角膜的脱水处理
IF 3.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-08-27 DOI: 10.1017/jfm.2024.416
Si Suo, Seyed Morteza Habibi Khorasani, Shervin Bagheri
In this study, we investigate the stability of a film that is attached to a corner between a cylinder and a substrate, using a combination of theoretical and numerical approaches. Notably, we place our focus on flat and thin films where the contact line is almost perpendicular to the cylinder wall whereas a small angle forms between the contact line and the substrate, and the film size is smaller than the cylinder radius. The film stability, which depends on the film size and the wall wettability, is first predicted by a standard linear stability analysis (LSA) within the long-wave theoretical framework. We find that the film size plays the most important role in controlling the film stability. Specifically, the thicker the film is, the less sensitive it becomes to the large-wavenumber perturbation. The wall wettability mainly impacts the growth rates of perturbations and slightly influences the marginal stability and postinstability patterns of wrapping films. We compare the LSA predictions with numerical results obtained from a disjoining pressure model (DPM) and volume-of-fluid (VOF) simulations, which provide more insights into the film breakup process. At the early stage there is a strong agreement between the LSA predictions and the DPM results. Notably, as the perturbation grows, thin film regions connecting two neighbouring satellite droplets form which may eventually lead to a stable or temporary secondary droplet, an aspect which the LSA is incapable of capturing. In addition, the VOF simulations suggest that beyond a critical film size, merging between two neighbouring drops becomes involved during the breakup stage. Therefore, the LSA predictions are able to provide only an upper limit on the final number of satellite droplets.
在本研究中,我们采用理论和数值相结合的方法,研究了附着在圆柱体和基体之间转角处的薄膜的稳定性。值得注意的是,我们将重点放在平薄薄膜上,即接触线几乎垂直于圆筒壁,而接触线与基底之间形成一个小角度,薄膜尺寸小于圆筒半径。薄膜稳定性取决于薄膜尺寸和壁面润湿性,我们首先在长波理论框架内通过标准线性稳定性分析 (LSA) 预测了薄膜稳定性。我们发现,薄膜尺寸在控制薄膜稳定性方面发挥着最重要的作用。具体来说,薄膜越厚,对大波长扰动的敏感性就越低。膜壁润湿性主要影响扰动的增长速度,对缠绕薄膜的边际稳定性和后不稳定性模式影响较小。我们将 LSA 预测结果与分离压力模型(DPM)和流体容积(VOF)模拟得出的数值结果进行了比较,从而对薄膜破裂过程有了更深入的了解。在早期阶段,LSA 预测结果与 DPM 结果非常一致。值得注意的是,随着扰动的增加,会形成连接两个相邻卫星液滴的薄膜区域,最终可能形成稳定或暂时的次级液滴,而 LSA 无法捕捉到这一点。此外,VOF 模拟表明,在超过临界薄膜尺寸后,两个相邻液滴之间的合并会在破裂阶段发生。因此,LSA 预测只能提供卫星液滴最终数量的上限。
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引用次数: 0
Understanding the effect of Prandtl number on momentum and scalar mixing rates in neutral and stably stratified flows using gradient field dynamics 利用梯度场动力学理解普朗特尔数对中性和稳定分层流中动量和标量混合率的影响
IF 3.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-08-27 DOI: 10.1017/jfm.2024.548
Andrew D. Bragg, Stephen M. de Bruyn Kops
Recently, direct numerical simulations (DNS) of stably stratified turbulence have shown that as the Prandtl number ( $Pr$ ) is increased from 1 to 7, the mean turbulent potential energy dissipation rate (TPE-DR) drops dramatically, while the mean turbulent kinetic energy dissipation rate (TKE-DR) increases significantly. Through an analysis of the equations governing the fluctuating velocity and density gradients we provide a mechanistic explanation for this surprising behaviour and test the predictions using DNS. We show that the mean density gradient gives rise to a mechanism that opposes the production of fluctuating density gradients, and this is connected to the emergence of ramp cliffs. The same term appears in the velocity gradient equation but with the opposite sign, and is the contribution from buoyancy. This term is ultimately the reason why the TPE-DR reduces while the TKE-DR increases with increasing $Pr$ . Our analysis also predicts that the effects of buoyancy on the smallest scales of the flow become stronger as $Pr$ is increased, and this is confirmed by our DNS data. A consequence of this is that the standard buoyancy Reynolds number does not correctly estimate the impact of buoyancy at the smallest scales when $Pr$ deviates from 1, and we derive a suitable alternative parameter. Finally, an analysis of the filtered gradient equations reveals that the mean density gradient term changes sign at sufficiently large scales, such that buoyancy acts as a source for velocity gradients at small scales, but as a sink at large scales.
最近,对稳定分层湍流的直接数值模拟(DNS)表明,当普朗特数($Pr$)从 1 增加到 7 时,平均湍流势能耗散率(TPE-DR)急剧下降,而平均湍流动能耗散率(TKE-DR)则显著增加。通过对波动速度梯度和密度梯度方程的分析,我们为这种令人惊讶的行为提供了机理解释,并利用 DNS 对预测结果进行了检验。我们发现,平均密度梯度产生了一种与波动密度梯度相反的机制,这与斜坡悬崖的出现有关。同样的项出现在速度梯度方程中,但符号相反,是浮力的贡献。这个项最终导致 TPE-DR 随着 $Pr$ 的增大而减小,而 TKE-DR 随着 $Pr$ 的增大而增大。我们的分析还预测,随着 Pr$ 的增加,浮力对最小尺度气流的影响会变得更强,我们的 DNS 数据也证实了这一点。其结果是,当 $Pr$ 偏离 1 时,标准浮力雷诺数不能正确估计浮力对最小尺度的影响,因此我们得出了一个合适的替代参数。最后,对滤波梯度方程的分析表明,平均密度梯度项在足够大的尺度上会改变符号,因此浮力在小尺度上是速度梯度的源,而在大尺度上则是速度梯度的汇。
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引用次数: 0
One-winged butterflies: mode selection for azimuthal magnetorotational instability by thermal convection 单翼蝴蝶:热对流方位磁定向不稳定性的模式选择
IF 3.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-08-27 DOI: 10.1017/jfm.2024.517
Ashish Mishra, George Mamatsashvili, Martin Seilmayer, Frank Stefani
The effects of thermal convection on turbulence in accretion discs, and particularly its interplay with the magnetorotational instability (MRI), are of significant astrophysical interest. Despite extensive theoretical and numerical studies, such an interplay has not been explored experimentally. We conduct linear analysis of the azimuthal version of MRI (AMRI) in the presence of thermal convection and compare the results with our experimental data published before. We show that the critical Hartmann number ( $Ha$ ) for the onset of AMRI is reduced by convection. Importantly, convection breaks symmetry between $m = pm 1$ instability modes ( $m$ is the azimuthal wavenumber). This preference for one mode over the other makes the AMRI wave appear as a ‘one-winged butterfly’.
热对流对吸积盘湍流的影响,特别是它与磁导不稳定性(MRI)的相互作用,具有重大的天体物理学意义。尽管进行了大量的理论和数值研究,但这种相互作用尚未得到实验探索。我们对存在热对流情况下的方位磁不稳定性(AMRI)进行了线性分析,并将结果与之前公布的实验数据进行了对比。我们的研究表明,对流会降低 AMRI 发生的临界哈特曼数($Ha$)。重要的是,对流打破了 $m =pm 1$ 不稳定模式($m$ 是方位角波数)之间的对称性。这种对一种模式的偏好使 AMRI 波看起来像一只 "单翼蝴蝶"。
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引用次数: 0
Turbulent jet theory via Lie symmetry analysis: the free plane jet 通过李对称分析的湍流射流理论:自由平面射流
IF 3.7 2区 工程技术 Q1 MECHANICS Pub Date : 2024-08-22 DOI: 10.1017/jfm.2024.527
Nadeem A. Malik, Fazle Hussain
A theory of incompressible turbulent plane jets (TPJs) is proposed by advancing an improved boundary layer approximation over the limiting classical – retaining more terms in the momentum balance equations. A pressure deficit inside the jet (with respect to the ambient) must exist due to transverse turbulence (Miller & Comings, <jats:italic>J. Fluid Mech.</jats:italic>, vol. 3, 1957, pp. 1–16; Hussain & Clarke, <jats:italic>Phys. Fluids</jats:italic>, vol. 20, 1977, pp. 1416–1426). Contrary to the universally accepted invariance of the total momentum flux <jats:inline-formula> <jats:alternatives> <jats:inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" mime-subtype="png" xlink:href="S0022112024005275_inline1.png"/> <jats:tex-math>$J_T(x)$</jats:tex-math> </jats:alternatives> </jats:inline-formula> (non-dimensionalized by its inlet value) as a function of the streamwise distance <jats:inline-formula> <jats:alternatives> <jats:inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" mime-subtype="png" xlink:href="S0022112024005275_inline2.png"/> <jats:tex-math>$x$</jats:tex-math> </jats:alternatives> </jats:inline-formula>, we prove that <jats:inline-formula> <jats:alternatives> <jats:inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" mime-subtype="png" xlink:href="S0022112024005275_inline3.png"/> <jats:tex-math>$J_T(x) >1$</jats:tex-math> </jats:alternatives> </jats:inline-formula> – a condition that all TPJs must satisfy; surprisingly, prior theories and most experiments do not satisfy this condition. This motivated us to apply Lie symmetry analysis with translational and dilatational transformations of the modified equations (incorporating <jats:inline-formula> <jats:alternatives> <jats:inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" mime-subtype="png" xlink:href="S0022112024005275_inline4.png"/> <jats:tex-math>$J_T>1$</jats:tex-math> </jats:alternatives> </jats:inline-formula>), which yields scaling laws for key jet measures: the mean streamwise and transverse velocities <jats:inline-formula> <jats:alternatives> <jats:inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" mime-subtype="png" xlink:href="S0022112024005275_inline5.png"/> <jats:tex-math>$U(x,y)$</jats:tex-math> </jats:alternatives> </jats:inline-formula> and <jats:inline-formula> <jats:alternatives> <jats:inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" mime-subtype="png" xlink:href="S0022112024005275_inline6.png"/> <jats:tex-math>$V(x,y)$</jats:tex-math> </jats:alternatives> </jats:inline-formula>, the turbulence intensities, the Reynolds shear stress <jats:inline-formula> <jats:alternatives> <jats:inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" mime-subtype="png" xlink:href="S0022112024005275_inline8.png"/> <jats:tex-math>$-rho ,overline {u'v'}(x,y)$</jats:tex-math> </jats:alternatives> </jats:inline-formula>, the mean pressure <jats:inline-formula> <jats:alternatives> <jats:inline-graphic xmlns:xlink="http://www.w3.org
提出了不可压缩湍流平面喷流(TPJs)理论,该理论通过改进边界层近似来超越传统的限制--在动量平衡方程中保留更多的项。由于横向湍流,喷流内部(相对于环境)必须存在压力不足(Miller & Comings,《流体力学》,第 3 卷,1957 年,第 1-16 页;Hussain & Clarke,《流体物理学》,第 20 卷,1977 年,第 1416-1426 页)。与普遍接受的总动量通量 $J_T(x)$(非以其入口值为维度)作为流向距离 $x$ 的函数的不变性相反,我们证明了 $J_T(x) >1$ - 所有 TPJ 都必须满足的条件;令人惊讶的是,先前的理论和大多数实验都不满足这个条件。这促使我们对修正方程(包含 $J_T>1$ )进行平移和扩张变换,应用李对称分析,从而得出关键射流量度的缩放定律:平均流向和横向速度 $U(x,y)$ 和 $V(x,y)$ 、湍流强度、雷诺切应力 $-rho ,overline {u'v'}(x,y)$ 、平均压力 $P(x,y)$ 等。满足 $J_T(x)>1$ 的实验验证了我们对所有射流测量值的预测,其中包括 $U$ 、$V$ 和 $-rhooverline {u'v'}$ 的剖面。我们进一步预测 $U sim x^{-0.24}$ 、 $V sim x^{-0.45}$ 、 $-rho ,overline {u'v'}sim x^{-0.69}$ 、质量通量 $Q_m sim x^{0.55}$ 以及 $J_T$ 会增加到大约 1.5。与经典的线性射流扩散相反,我们发现了亚线性扩散,射流半宽的增长速度为$b(x)sim x^{0.79}$,表明射流更窄。我们的预测与文献报道的大多数结果明显不同。这些矛盾要求我们重新审视涉及精心设计的设施和边界条件以及高分辨率模拟的射流研究。
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Journal of Fluid Mechanics
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