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The effect of elevated initial vortex shapes on its evolution 初始旋涡形状升高对其演变的影响
IF 1.5 4区 工程技术 Q3 MECHANICS Pub Date : 2023-04-14 DOI: 10.1088/1873-7005/accd17
A. Elikashvili, E. Golbraikh
The formation and evolution of helical vortices in various media is an important hydrodynamic problem. A separate problem is the study of the behavior of the initial vortex, which is elevated above the surface. The evolution of such vortices is a complex multiparameter phenomenon. Based on a simple hydrodynamic model (or minimal model) in Elikashvili et al (2017 Phys. Fluids 29 026602) have been studied the formation of vorticity near the surface as a function of the initial height of the vortex and the Reynolds number. However, the influence of the parameters of the initial vortex profile on its evolution was not considered. In this paper, based on a simple hydrodynamic model, we study the evolution and formation of vortices near a solid surface for various initial vorticity profiles. The most widespread vortex profiles of Rankine, Burgers, and Vatistas were chosen for research. The simulation shows that the evolution of the vortex depends on its initial profile.
螺旋涡在各种介质中的形成和演化是一个重要的流体动力学问题。一个单独的问题是研究初始涡流的行为,它被提升到表面以上。这种旋涡的演化是一个复杂的多参数现象。基于Elikashvili等人(2017 Phys.Fluids 29 026602)中的一个简单流体动力学模型(或最小模型),研究了表面附近涡度的形成,该涡度是涡流初始高度和雷诺数的函数。然而,没有考虑初始涡流剖面参数对其演变的影响。本文基于一个简单的流体动力学模型,研究了不同初始涡度剖面下固体表面附近旋涡的演化和形成。选择兰金、伯格和瓦蒂斯塔斯分布最广的涡旋剖面进行研究。模拟结果表明,旋涡的演化取决于其初始轮廓。
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引用次数: 0
Viscous flow through macroscopic spherical cavities in an arbitrary configuration in a granular material 颗粒材料中任意形状宏观球形空腔中的粘性流动
IF 1.5 4区 工程技术 Q3 MECHANICS Pub Date : 2023-02-24 DOI: 10.1088/1873-7005/acbedb
O. Sano
Viscous flow through macroscopic spherical cavities in a granular material is theoretically investigated. Number, size and configuration of the cavities are arbitrary, except that cavities are sufficiently distant to allow asymptotic analysis on their interaction, which is taken into account up to O(a/l)3 , where a and l are the characteristic radius and inter-cavity distance, respectively. Dependence of the flow field, flux into respective cavities and stress field etc on the cavity size, separation distance and orientation are analyzed. As further examples, 1D-, 2D-, and 3D-array of equal size cavities are examined, by which onset of the collapse of cavity and development of the collapsed region are elucidated. The latter may predict landslides and other flow-induced catastrophic changes in the material with quasi-equilibrium solid structure, as well as microscale waterway formation in human tissue known as angiogenesis.
从理论上研究了颗粒状材料宏观球腔中的粘性流动。空腔的数量、大小和结构是任意的,除了空腔足够远,可以对它们的相互作用进行渐近分析,这被考虑到O(a/l)3,其中a和l分别是特征半径和腔间距离。分析了腔体尺寸、分离距离和方向对流场、进入腔体的通量和应力场等的影响。作为进一步的例子,研究了等尺寸空腔的1D, 2D和3d阵列,通过它们阐明了空腔塌陷的开始和塌陷区域的发展。后者可以预测具有准平衡固体结构的物质中的滑坡和其他由水流引起的灾难性变化,以及被称为血管生成的人体组织中的微尺度水道形成。
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引用次数: 0
Numerical analysis of shock characteristics control based on bump 基于碰撞的冲击特性控制数值分析
IF 1.5 4区 工程技术 Q3 MECHANICS Pub Date : 2023-02-10 DOI: 10.1088/1873-7005/acbb22
Dawei Li, Kaibo Yu, X. Wang, Yuan-bo Gao
The effects of bump control on shock aerodynamic characteristics have been investigated by simulations. A bump control that based on the changes of local upper surface of two-dimensional (2D) airfoil or three-dimensional (3D) wing model has been applied to affect the shock intensity and position. The simulation results are close of other experiment when the calculate parameters are same with each other. The simulations show that the drag and lift characteristics can be improved with the bump control, and the results of improvement strongly depend on control parameters. For the 2D RAE2822 airfoil, the optimal control position of the bump control must keep close to the position of the shock wave. The 3D local bump that located on 80% wing span wise and closed to the tip can acquire a batter control results for the 3D RAE2822 wing model.
通过仿真研究了碰撞控制对冲击气动特性的影响。基于二维(2D)机翼或三维(3D)机翼模型的局部上表面的变化,应用了一种碰撞控制来影响冲击强度和位置。当计算参数相同时,仿真结果与其他实验结果接近。仿真结果表明,凸块控制可以改善阻力和升力特性,并且改善效果与控制参数密切相关。对于2D RAE2822翼型,撞击控制的最佳控制位置必须保持接近冲击波的位置。位于80%翼展方向并靠近尖端的3D局部凸起可以获得3D RAE2822机翼模型的倾斜控制结果。
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引用次数: 0
A full-Eulerian approach for simulation of a system of fluid–rigid–elastic structure interaction based on the vorticity-stream function formulation 基于涡度流函数公式的流体-刚性-弹性结构相互作用系统模拟的全欧拉方法
IF 1.5 4区 工程技术 Q3 MECHANICS Pub Date : 2023-02-08 DOI: 10.1088/1873-7005/acba44
I. Farahbakhsh, Amin Paknejad, H. Ghassemi
A monolithic mathematical framework for understanding the fluid–rigid–elastic structure interaction problem is proposed. A numerical method in a secondary formulation of the Navier–Stokes equations accompanying a technique for imposing the rigid boundaries is applied. The one-fluid formulation of the incompressible Navier–Stokes equation, containing the terms governing the elastic structure, is transformed into the vorticity-stream function formulation. The rigid structure is imposed in the flow field based on the velocity–vorticity kinematic relation and harmonic function theorem. The vorticity, level-set function, and left Cauchy–Green deformation tensor are updated utilizing three transport equations to investigate the evolution of the velocity field, elastic structure(s) configuration, and elastic stress tensor. The method is implemented to solve three challenging problems, and the results show its capabilities in proper imposing the rigid structures in the flow field and also the simultaneous modeling the rigid and elastic structure interactions with incompressible fluid flow.
提出了一个理解流体-刚性-弹性结构相互作用问题的整体数学框架。在Navier–Stokes方程的二次公式中应用了一种数值方法,该方法伴随着施加刚性边界的技术。不可压缩Navier-Stokes方程的单流体公式,包含控制弹性结构的项,被转换为涡流函数公式。基于速度-涡度运动学关系和调和函数定理,在流场中施加刚性结构。利用三个输运方程更新涡度、水平集函数和左柯西-格林变形张量,以研究速度场、弹性结构配置和弹性应力张量的演变。该方法用于解决三个具有挑战性的问题,结果表明,该方法能够在流场中正确地施加刚性结构,并同时模拟刚性和弹性结构与不可压缩流体流的相互作用。
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引用次数: 1
Three-dimensional numerical study of acoustic streaming phenomenon in rectangular resonator 矩形谐振腔中声流现象的三维数值研究
IF 1.5 4区 工程技术 Q3 MECHANICS Pub Date : 2023-01-13 DOI: 10.1088/1873-7005/acb2f7
Z. Malecha
The article presents a three-dimensional numerical study of the large-amplitude, acoustically driven streaming flow in rectangular resonator for different frequencies of the acoustic wave and different temperature regime, isothermal and 60 K temperature difference between the top and bottom walls. The utilized numerical model was based on the Navier–Stokes compressible equations, the ideal gas model, and finite volume discretization. The oscillating wall of the resonator was modeled as a dynamically moving boundary of the numerical domain. The size of the resonators was adjusted to fit one period of the acoustic wave. The research revealed a stationary pair of streaming vortices in the resonator with a characteristic three-dimensional structure. Their intensity was much greater in the case of nonisothermal flow. The study of the impact of side walls on the intensity of streaming revealed its gradual decrease with approaching the walls, creating a quasiparabolic profile in the resonator. Interestingly, the relationship between the intensity of streaming and the frequency of the acoustic wave turned out to be not trivial and two maxima for different frequencies could be observed.
本文对矩形腔内不同声波频率、不同温度、等温及上下壁面60k温差下的大振幅声驱动流场进行了三维数值研究。所采用的数值模型基于Navier-Stokes可压缩方程、理想气体模型和有限体积离散。将谐振腔的振荡壁建模为数值域的动态移动边界。调整谐振器的尺寸以适应声波的一个周期。研究发现谐振腔中存在一对具有三维结构特征的静止流涡。在非等温流动中,它们的强度要大得多。研究了侧壁对流场强度的影响,发现流场强度随着靠近侧壁逐渐减小,在谐振腔内形成了准抛物线型。有趣的是,流强度与声波频率之间的关系并非微不足道,在不同频率下可以观察到两个最大值。
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引用次数: 1
Mass transport in oscillatory electroosmotic viscoelectric flow in a hydrophobic microchannel with steric effect 具有空间效应的疏水微通道中振荡电渗透粘电流动的质量传递
IF 1.5 4区 工程技术 Q3 MECHANICS Pub Date : 2023-01-09 DOI: 10.1088/1873-7005/acb170
R. Baños, J. Arcos, O. Bautista, F. Méndez
We conduct a numerical study of viscoelectric and steric effects on an oscillatory electroosmotic flow (OEOF) and their impact on the mass transport of a passive solute through a hydrophobic microchannel. In many applications of electroosmosis, zeta potentials as high as 100–200 mV can be found; in such a situation, the Debye–Hückel approximation is no longer valid, and the steric effect must be considered because the crowding of finite-sized ions close to the microchannel walls. In addition to the previous effect, the local viscosity can be increased due to the viscoelectric effect for strong electric potentials induced in the electric double layer. Earlier works have studied the mass transfer caused by an OEOF; however, the combined effects’ influence has not been considered. This research suggests that under an appropriate combination of the viscoelectric and steric effects, together with the microchannel hydrophobicity, the mass transport can be controlled and notably enhanced compared with the case where such effects are disregarded. An interesting behavior occurs for relatively high values of the steric factor ν, where there is a linear dependence between the mass transport Q˜ and the viscoelectric factor f˜ ; in contrast, for low values of ν, the relationship Q˜−f˜ is non-linear.
我们对振荡电渗流(OEOF)的粘电效应和空间效应及其对被动溶质通过疏水微通道的质量传输的影响进行了数值研究。在电渗的许多应用中,ζ电位高达100–200 可以找到mV;在这种情况下,Debye–Hückel近似不再有效,必须考虑空间效应,因为有限尺寸的离子靠近微通道壁。除了先前的效应之外,由于双电层中感应的强电势的粘电效应,局部粘度可以增加。早期的工作已经研究了OEOF引起的传质;然而,综合效应的影响没有被考虑在内。这项研究表明,在粘电效应和空间效应以及微通道疏水性的适当组合下,与忽略这些效应的情况相比,质量传输可以得到控制并显著增强。对于相对较高的空间因子Γ值,发生了一种有趣的行为,其中质量输运Q~和粘电因子f~之间存在线性相关性;相反,对于低值的Γ,关系Q~−f~是非线性的。
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引用次数: 0
Rheology, rheometers, and matching models to experiments 流变学,流变仪,和匹配模型的实验
IF 1.5 4区 工程技术 Q3 MECHANICS Pub Date : 2023-01-03 DOI: 10.1088/1873-7005/acafa1
L. R. Scott
We consider the general problem of matching rheological models to experiments. We introduce the concept of identifiability of models from a given set of experiments. To illustrate this in detail, we study two rheology models, the grade-two and Oldroyd 3-parameter models, and consider two hypothetical rheometers to see if the coefficients of the rheology models are identifiable from experimental measurements or not. For the Oldroyd models, we show that the coefficients can be estimated from experiments from the two rheometers. But for the grade-two model, it is not possible to distinguish the two nonNewtonian parameters, only their sum can be estimated, and thus the grade-two model is not identifiable by the two hypothetical rheometers. However, our results imply that a different rheometer may be able to do that.
我们考虑将流变模型与实验相匹配的一般问题。我们从一组给定的实验中引入模型可辨识性的概念。为了详细说明这一点,我们研究了两种流变模型,grade- 2和Oldroyd 3参数模型,并考虑了两种假设流变仪,看看流变模型的系数是否可以从实验测量中识别出来。对于Oldroyd模型,我们证明了系数可以从两个流变仪的实验中估计出来。但对于二级模型,无法区分两个非牛顿参数,只能估计它们的和,因此二级模型无法通过两个假设流变仪识别。然而,我们的结果表明,一种不同的流变仪可能能够做到这一点。
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引用次数: 0
Numerical simulation of vortex shedding from rectangular cylinders with different elongation ratios 不同伸长率矩形圆柱体旋涡脱落的数值模拟
IF 1.5 4区 工程技术 Q3 MECHANICS Pub Date : 2023-01-03 DOI: 10.1088/1873-7005/acafa0
Jian Wu, Yakun Liu, Di Zhang, Ze Cao, Zhuoyue Li
RANS simulations are performed for flow past rectangular cylinders with different elongation ratios (L/D= 1, 2, 4, 6, 8, 10, 12, 14 and 16) at Re= 22 000 using the k-ω SST turbulence model. As L/D increases from 1 to 6, stepwise increase of Strouhal number (St) exists, whereas an almost linear variation of St with respect to L/D can be found (St= 0.1618*L/D) at L/D⩾ 8. In the flow, two small secondary vortices beneath the shear layers are identified and the trailing-edge secondary vortex presents opposite rotational direction comparing with the leading-edge main vortex. Analysis of the shear layer and vortex characteristics is carried out to correlate with the wall normal stress and shear stress on the rectangular cylinder surfaces. Further, four coupling modes between leading-edge vortex (L-vortex) and trailing-edge vortex (T-vortex) among cylinders with different L/D are observed, named L-Vortex Mode (i.e. L/D= 1–2), L-T-Vortex Mode (i.e. L/D= 4–8), T-L-Vortex Mode (i.e. L/D= 10–14), and T-Vortex Mode (i.e. L/D ⩾ 16). When L/D > 4, the convective velocity of the L- and T-vortex is not sensitive to the L/D.
在Re=22时,对经过具有不同伸长率(L/D=1、2、4、6、8、10、12、14和16)的矩形圆柱体的流动进行了RANS模拟 000,使用k-ωSST湍流模型。当L/D从1增加到6时,存在斯特劳哈尔数(St)的逐步增加,而在L/D⩾8时,可以发现St相对于L/D的几乎线性变化(St=0.1618*L/D)。在流动中,识别出剪切层下方的两个小的二次涡,后缘二次涡与前缘主涡相比呈现相反的旋转方向。对剪切层和涡流特性进行了分析,以将矩形圆柱体表面的壁面法向应力和剪切应力关联起来。此外,在不同L/D的气缸之间,观察到了前缘涡流(L涡流)和后缘涡流(T涡流)之间的四种耦合模式,分别命名为L涡流模式(即L/D=1–2)、L-T涡流模式(如L/D=4–8)、T-L涡流模式(即L/D=10–14)和T涡流模式。当L/D>4时,L涡和T涡的对流速度对L/D不敏感。
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引用次数: 1
A unified model of suspension concentration distribution in sediment mixed turbulent flows using generalized fractional advection-diffusion equation 基于广义分数平流扩散方程的泥沙混合湍流悬浮液浓度分布统一模型
IF 1.5 4区 工程技术 Q3 MECHANICS Pub Date : 2022-12-19 DOI: 10.1088/1873-7005/acacc1
S. Kundu, Ravi Ranjan Sinha
The fractional operator in a space fractional advection-diffusion equation (FADE) plays a significant role in the mixing and vertical movement of sediment particles in a sediment-laden turbulent flow under non-local effects. Turbulent flow exhibits non-local mixing properties, which leads to the non-Fickian diffusion process that cannot be captured by the traditional diffusion equation. In this work, we present a generalized FADE that includes the generalized fractional differential operator in the Caputo sense. The full analytical solution is proposed utilizing the general Laplace transformation method. This generalized solution contains weight and scale functions and includes the effects of non-locality. It has been shown that several existing famous models of suspension concentration distribution for sediment particles (including both type-I and type-II distributions) in turbulent flows can be obtained from the proposed generalized solution with proper choices of the scale and weight functions in particular. Here a total of fourteen different types of concentration distribution equations including type-I and type-II profiles are derived from the general solution. Further possible generalizations of the model are also discussed which are more useful for practical applications. It is found that the several existing sediment distribution models are equivalent up to choices of weight and scale functions. Further, we found that the scale function could be physically related to the characteristic Lagrangian length of sediment mixing. The choice of the scale and weight function for both the type-I and type-II profiles are discussed and analyzed. Finally, the model is validated with experimental data as well as field data from the Missouri River, Mississippi River, and Rio Grande conveyance channels, and in each case, satisfactory agreements are obtained. These suggest the broader applicability of the present study.
空间分数平流-扩散方程(FADE)中的分数算子在非局部效应下泥沙颗粒在含沙湍流中的混合和垂直运动中起着重要作用。湍流表现出非局部混合特性,这导致了传统扩散方程无法捕捉到的非菲基扩散过程。在这项工作中,我们提出了一个广义FADE,它包括Caputo意义上的广义分数微分算子。利用一般的拉普拉斯变换方法给出了完整的解析解。该广义解包含权函数和标度函数,并包含非局部性的影响。研究表明,在适当选择尺度函数和权重函数的情况下,从所提出的广义解可以获得湍流中泥沙颗粒悬浮浓度分布的几个著名模型(包括I型和II型分布)。这里,从通解中导出了总共十四种不同类型的浓度分布方程,包括I型和II型剖面。还讨论了该模型的进一步可能推广,这些推广对实际应用更有用。研究发现,现有的几种泥沙分布模型在重量函数和比例函数的选择上是等效的。此外,我们发现尺度函数可能与沉积物混合的特征拉格朗日长度存在物理关系。讨论和分析了I型和II型剖面的比例和权重函数的选择。最后,用实验数据以及密苏里河、密西西比河和格兰德河输送通道的现场数据对模型进行了验证,在每种情况下都获得了令人满意的一致性。这表明本研究具有更广泛的适用性。
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引用次数: 0
The wake of a rectangular flat plate 矩形平板的尾流
IF 1.5 4区 工程技术 Q3 MECHANICS Pub Date : 2022-12-15 DOI: 10.1088/1873-7005/acabe3
E. Montes Gomez, D. Sumner
The mean wake of a three-dimensional surface-mounted rectangular flat plate was studied experimentally in a low-speed wind tunnel for four different aspect (height-to-width) ratios, AR = 3, 2, 1, and 0.5. The Reynolds number based on the plate width was Re = 3.8 × 104 and the boundary layer thickness on the ground plane, relative to the plate width, was δ/W = 1.1. The incidence angle of the plate was varied from α = 0° (where the plate is normal to the flow) to α = 90° (where the plate is parallel to the flow). The mean velocity and vorticity fields in the wake were measured using a seven-hole pressure probe. At α = 0°, the length of the recirculation zone behind the plate becomes progressively shorter as the aspect ratio is lowered and follows the same tendency as that of a finite square prism. The wakes of the slenderer flat plates of AR = 3 and 2 are characterised by two pairs of streamwise vortices: a pair of tip vortices in the upper wake and a pair of ground-plane vortices on the lower edges of the wake. With increasing incidence angle, a single tip vortex comes to dominate the wake, secondary vorticity is induced at various locations, a ‘traffic light’ vortex pattern may form, and ultimately a familiar wing-tip (trailing) vortex develops. In contrast, flow downstream of the less slender flat plates of AR = 1 and 0.5 is characterised by a single pair of large streamwise vortices, which become asymmetric with increasing incidence. Close to the flat plate of AR = 0.5, and at small incidence angles only, a unique pair of small inner vorticity concentrations, of opposite sense of rotation to the main streamwise vortices, is found in the upper part of the wake.
在低速风洞中对四种不同纵横比(高宽比)的三维表面安装矩形平板的平均尾流进行了实验研究,AR=3、2、1和0.5。基于板宽度的雷诺数为Re=3.8×104,相对于板宽度,地平面上的边界层厚度为δ/W=1.1。板的入射角从α=0°(板垂直于流)到α=90°(板平行于流)不等。尾流中的平均速度场和涡度场是用七孔压力探针测量的。在α=0°时,随着纵横比的降低,板后再循环区的长度逐渐变短,并遵循与有限方棱镜相同的趋势。AR=3和2的细长平板的尾流由两对流向涡流表征:尾流上部的一对尖端涡流和尾流下部边缘的一对地平面涡流。随着入射角的增加,单梢涡流开始主导尾流,在不同位置产生二次涡度,可能形成“红绿灯”涡流模式,最终形成熟悉的翼尖(后缘)涡流。相反,AR=1和0.5的较不细长平板下游的流动以一对大的顺流涡流为特征,这些涡流随着入射角的增加而变得不对称。在AR=0.5的平板附近,仅在较小的入射角下,在尾流的上部发现了一对独特的小内涡浓度,其旋转方向与主流向涡相反。
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引用次数: 0
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Fluid Dynamics Research
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