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Continuum Modeling and Numerical Simulation of Active Suspensions in Curved Channels 弯曲河道主动悬架的连续体建模与数值模拟
IF 2.8 3区 工程技术 Q2 MECHANICS Pub Date : 2025-08-19 DOI: 10.1007/s00162-025-00752-2
Houssem Ben Gozlen, Yongqi Wang, Martin Oberlack

This paper presents a two-fluid model to simulate the behavior of uniformly oriented active suspensions in curved annular channels. Active suspensions consist of self-propelled particles suspended in a fluid that exhibit complex collective behavior through interactions with their surrounding environment. The proposed model captures key interactions between the fluid and particle phases, including drag and lift forces, and allows the analysis of flow patterns and particle distributions. The study investigates the flow of active suspensions in an annular channel with a rectangular cross-section, where stable secondary flow patterns develop, characterized notably by Dean vortices. Numerical simulations are used to examine the effects of channel curvature and aspect ratio on the dynamics of these suspensions. Results reveal that increased curvature intensifies the formation of Dean vortices, which significantly affect the particle distribution. Additionally, larger aspect ratios increase the strength of the secondary flow and enhance particle segregation. Model comparison to direct numerical simulations shows a qualitatively good agreement in predicting particle distribution profiles.

本文提出了一种双流体模型来模拟均匀定向主动悬架在弯曲环形通道中的行为。主动悬架由悬浮在流体中的自推进粒子组成,这些粒子通过与周围环境的相互作用表现出复杂的集体行为。所提出的模型捕获了流体和颗粒相之间的关键相互作用,包括阻力和升力,并允许分析流动模式和颗粒分布。该研究研究了主动悬液在矩形截面环形通道中的流动,在环形通道中,稳定的二次流模式发展,其特征是Dean涡。数值模拟研究了通道曲率和纵横比对这些悬架动力学的影响。结果表明,增大的曲率加剧了Dean涡的形成,对颗粒分布有显著影响。此外,较大的展弦比增加了二次流的强度,并增强了颗粒的偏析。模型与直接数值模拟的比较表明,在预测颗粒分布剖面方面具有较好的一致性。
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引用次数: 0
Analysis of MHD stokes fluid flow in a cavity driven by moving parallel lid(s) 移动平行顶盖驱动的MHD stokes腔内流体流动分析
IF 2.8 3区 工程技术 Q2 MECHANICS Pub Date : 2025-08-04 DOI: 10.1007/s00162-025-00750-4
Mustafa Turkyilmazoglu, Abdulaziz Alotaibi

Controlling cavity flow through an effective magnetic field is highly desirable in many engineering applications. This work addresses the analytical solution for arbitrary depth cavity flow driven by two parallel lids under the influence of a uniform magnetic field acting along the x, y, or z axes, within the Stokes flow approximation. The formation of creeping flow and associated vortices is separated into symmetric and anti-symmetric modes, then combined to create the desired final cavity motion. The linear biharmonic equation of the stream function, modified by a Lorentz force term, is solved by constructing relevant real eigenvalues and eigenfunctions for both modes. This eigen-decomposition allows for the solution of algebraic linear equations for the coefficients in the series expansions, eliminating the need for numerical computations. This offers a significant advantage over the commonly used Papkovich-Faddle method. Our non-magnetic flow results precisely reproduce the dynamics available in the literature, primarily obtained through numerical simulations. Similarly, the MHD flow results derived from our analysis successfully replicate the numerical data found in the literature, with the exception of some ambiguous published data. These findings covering a range of Hartmann numbers between 0 and 80 valid for numerous cavity depths are further validated by finite element simulations conducted in Mathematica software, highlighting the value of the analytical solutions in discerning actual data from ambiguous information. The presented analytical solutions offer valuable physical insights into the vortical behavior of rectangular cavity motion under moderate and strong magnetic fields. The formulae clearly illustrate the breakup of the main recirculating zone, the centerline velocity structure, the core of the vortices, and the formation of boundary layers. These insights can be leveraged to determine the preferred magnetic field direction for optimal control of the cavity flow.

在许多工程应用中,通过有效的磁场来控制空腔流动是非常可取的。在Stokes流近似中,本工作解决了在沿x、y或z轴作用的均匀磁场影响下,由两个平行盖驱动的任意深度腔流的解析解。蠕动流动和相关漩涡的形成被分为对称和反对称模式,然后结合在一起,形成所需的最终空腔运动。通过构造两种模态的相关实特征值和特征函数,求解了经洛伦兹力项修正的流函数的线性双调和方程。这种特征分解允许求解级数展开中系数的代数线性方程,从而消除了数值计算的需要。与常用的Papkovich-Faddle方法相比,这提供了一个显著的优势。我们的非磁流结果精确地再现了文献中可用的动力学,主要是通过数值模拟获得的。同样,从我们的分析中得出的MHD流动结果成功地复制了文献中发现的数值数据,除了一些模棱两可的已发表数据。这些发现涵盖了0到80之间的哈特曼数范围,适用于许多空腔深度,并通过Mathematica软件进行的有限元模拟进一步验证,突出了分析解决方案在从模糊信息中识别实际数据方面的价值。本文给出的解析解对中强磁场下矩形空腔运动的涡旋特性提供了有价值的物理见解。该公式清楚地说明了主环流带的解体、中心线速度结构、涡核和边界层的形成。这些见解可以用来确定最佳控制腔流的首选磁场方向。
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引用次数: 0
Direct numerical simulation of flow past a Gaussian bump at a high Reynolds number 高雷诺数下流过高斯凸起的直接数值模拟
IF 2.8 3区 工程技术 Q2 MECHANICS Pub Date : 2025-07-14 DOI: 10.1007/s00162-025-00749-x
Ali Uzun, Mujeeb R. Malik

We present the results from a direct numerical simulation of a spanwise-periodic turbulent flow past a Gaussian bump. The problem setup is designed to investigate the interaction of an incoming turbulent boundary layer with the strong favorable and adverse pressure gradients generated by the Gaussian bump as the flow passes over it at a Reynolds number of 340000 based on the bump height, or 4 million based on the bump length. The statistical results from the present simulation are compared against our earlier results at a Reynolds number of 2 million. An internal layer, which forms beneath the strongly accelerated boundary layer over the windward side of the bump, is found to generate its near-wall turbulence stress peaks in closer proximity of the wall in the higher Reynolds-number case. Furthermore, the logarithmic layer of the higher Reynolds-number boundary layer appears more resistant to changes induced by strong acceleration and surface curvature effects over the same region. Despite a nearly identical flow separation point in the two flows, the detached shear layer grows at a faster rate and subsequently reattaches at an earlier point in the higher Reynolds-number flow. The surface pressure and skin-friction distributions over the attached flow region compare well against the corresponding experimental data for both flows. However, some differences appear in the separated flow region, which are attributed to the three-dimensionality of the experimental model setup that is not included in the simulation owing to the spanwise periodic assumption. Comparisons with the stereoscopic particle image velocimetry measurements on the central plane of the experimental model over the windward side of the bump show reasonable overall agreement in the mean velocity components, but the turbulence stress components do not agree well at some streamwise locations. Comparisons over the leeward side of the bump show that the mean separated shear layer in the simulation is tilted significantly more toward the wall than the experimental shear layer on the central plane. This mismatch in the mean shear layer orientation is due to the experimental model three-dimensionality and tunnel end-wall effects, which are not modeled in the present spanwise-periodic simulation.

我们提出了一个直接数值模拟的结果,从一个展向周期湍流流过高斯凹凸。问题设置旨在研究湍流边界层与高斯凸起产生的强有利和不利压力梯度的相互作用,当气流以凸起高度为340000的雷诺数或凸起长度为400万的雷诺数通过它时。在雷诺数为200万的情况下,本模拟的统计结果与我们之前的结果进行了比较。在高雷诺数的情况下,在碰撞迎风面的强加速边界层下形成的内层在靠近壁面的地方产生了近壁湍流应力峰值。此外,在同一区域内,高雷诺数边界层的对数层对强加速度和表面曲率效应引起的变化表现出更强的抵抗力。尽管在两种流动中有几乎相同的流动分离点,但在高雷诺数流动中,分离的剪切层以更快的速度生长,随后在更早的点重新附着。附着流区的表面压力和表面摩擦分布与两种流动的相应实验数据比较良好。然而,在分离的流动区域出现了一些差异,这是由于实验模型设置的三维性,由于展向周期假设而没有包括在模拟中。与实验模型迎风面中心平面上的立体粒子图像测速结果比较,平均速度分量总体上比较一致,但湍流应力分量在一些流向位置不太一致。在凸起背风侧的对比表明,模拟中平均分离剪切层比实验剪切层在中心平面上更倾向于壁面。这种平均剪切层方向的不匹配是由于实验模型的三维和隧道端壁效应,而这些在目前的展向周期模拟中没有被模拟。
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引用次数: 0
Effect of rounded trailing edges on unsteady airfoil loading at low reynolds numbers 低雷诺数下圆形尾缘对非定常翼型载荷的影响
IF 2.8 3区 工程技术 Q2 MECHANICS Pub Date : 2025-07-05 DOI: 10.1007/s00162-025-00747-z
Yi Tsung Lee, Kiran Ramesh, Ashok Gopalarathnam

The steady potential flow past a traditional airfoil with a round leading edge and a sharp trailing edge can usually be simulated using the assumption of Kutta condition at the trailing edge. However, for the airfoil undergoing unsteady motion, especially at high reduced frequencies, numerical and experimental studies have shown that the flow can curve around the trailing edge, resulting in the stagnation point moving away from the trailing edge. This phenomenon becomes increasingly apparent when the airfoil has a round trailing edge instead of the usual sharp one. Inspired by the success of using leading-edge suction force to represent the flow turn-around at the leading edge and the associated vortex shedding, this work introduces the trailing-edge suction force and connects it to the trailing-edge unsteady flow physics. In this work, the effect of trailing edge roundness on the unsteady airfoil flow is studied by generating airfoil shapes with various amounts of roundness. Computational fluid dynamics (CFD) studies of unsteady flow past airfoils with different round trailing edges are performed to study the effects of the trailing-edge suction force on the flowfield. A composite pressure-difference model, universally valid on the entire airfoil, is derived in this work to take into account the edge radii and the corresponding edge-suction effects. We show that, in scenarios where the stagnation point moves away from the trailing edge, a trailing-edge suction force, associated with the flow curving around the trailing edge, is necessary to better estimate the airfoil unsteady load distribution.

传统圆前缘锐后缘翼型的定常势流通常采用后缘库塔条件进行模拟。然而,对于非定常运动的翼型,特别是在高降频下,数值和实验研究表明,流动可以在尾缘周围弯曲,导致驻点远离尾缘。这种现象变得越来越明显,当翼型有一个圆形的后缘,而不是通常的尖锐的一个。受前缘吸力成功表示前缘回转和相关涡脱落的启发,本文引入了尾缘吸力,并将其与尾缘非定常流物理联系起来。在这项工作中,研究了后缘圆度对非定常翼型流动的影响,产生了不同圆度的翼型形状。采用计算流体力学方法对不同圆形尾缘的非定常流场进行了研究,研究了尾缘吸力对流场的影响。考虑翼型边缘半径和相应的边缘吸力效应,推导了一种普遍适用于整个翼型的复合压差模型。我们表明,在滞止点远离尾缘的情况下,与尾缘周围流动曲线相关的尾缘吸力对于更好地估计翼型非定常负载分布是必要的。
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引用次数: 0
Crystal-like arrangements of knotted or linked vortex tubes in hexagonal Beltrami flows 六边形贝尔特拉米流中结结或连接的漩涡管的晶体状排列
IF 2.8 3区 工程技术 Q2 MECHANICS Pub Date : 2025-07-01 DOI: 10.1007/s00162-025-00748-y
Takahiro Nishiyama

When knotted or linked vortex tubes are considered in real-analytic steady Euler flows, the flows should be Beltrami flows with constant proportionality factors that have chaotic streamlines. In this study, four types of such Beltrami flows were derived on the assumption that the set of streamlines in each flow had hexagonal symmetry. Their systematic derivation was enabled by information provided via crystallography, which is applicable to spatially periodic objects not restricted to chemical materials. Invariant tori, which are stream and vortex tubes in Beltrami flows, were numerically investigated using various proportionality factors and initial points for the derived hexagonal flows. As a result, a variety of knotted or linked invariant tori were found to be arranged as atoms in hexagonal crystals. Some invariant tori were observed to form infinitely spreading chains with link structures similar to those of chain-mail-like polycatenanes in chemistry.

在实解析稳定欧拉流中考虑结涡管或连接涡管时,该流应是具有恒定比例因子的具有混沌流线的Beltrami流。在本研究中,假设每个流中的流线集具有六边形对称性,推导出四种类型的Beltrami流。它们的系统推导是通过晶体学提供的信息实现的,晶体学适用于不限于化学材料的空间周期性物体。用不同的比例因子和初始点对推导出的六边形流进行了数值研究,其中不变环面是Beltrami流中的流管和涡管。结果,发现了各种结的或连接的不变环面在六方晶体中以原子的形式排列。观察到一些不变环面形成无限伸展的链,其连接结构类似于化学中的链状聚链环。
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引用次数: 0
Vortex equilibria using least-squares methods 用最小二乘法求解涡旋平衡。
IF 2.8 3区 工程技术 Q2 MECHANICS Pub Date : 2025-06-28 DOI: 10.1007/s00162-025-00746-0
Samuel J. Harris, N. R McDonald

Numerical methods and results for computing rotating or stationary equilibria of vortex patches and sheets, some in the presence of point vortices, are presented. The methods are based on those recently developed by Trefethen and colleagues for solving Laplace’s equation in the complex plane by series and rational approximation. They share the common feature of finding the coefficients of the approximation by the fitting of boundary conditions using least-squares. Application of these methods to vortex patches requires their extension to the solution of Poisson’s and Laplace’s equation in two domains with matching conditions across the patch boundary. In the case of vortex sheets, the streamlines of the solution are computed along with the circulation density of the sheet. The use and accuracy of the methods is demonstrated by reproducing known results for equilibrium patches and vortex sheets, some having point vortices present. Several new numerical equilibrium solutions are also computed: a single straight sheet with two and four satellite point vortices respectively, and a three-sheeted structure, with the sheets emanating from a common point of rotation. New numerical solutions are also found for steady, doubly-connected vortex layers of uniform vorticity surrounding solid objects and such that the fluid velocity vanishes on the outer free boundary.

本文给出了计算涡块和涡片旋转或静止平衡的数值方法和结果,其中一些是在点涡存在的情况下。这些方法是基于Trefethen及其同事最近开发的用级数和有理逼近法在复平面上求解拉普拉斯方程的方法。它们的共同特点是用最小二乘拟合边界条件求得近似的系数。将这些方法应用于涡旋斑块,需要将其扩展到两个域的泊松方程和拉普拉斯方程的解,并在两个域上跨越斑块边界具有匹配条件。在涡旋片的情况下,溶液的流线随片的循环密度计算。通过对平衡块和涡片(其中一些有点涡)的已知结果的再现,证明了该方法的使用和准确性。本文还计算了几种新的数值平衡解:分别具有两个和四个卫星点涡的单直片结构,以及从一个共同旋转点发出的三片结构。对于固体周围具有均匀涡量且流体速度在自由边界上消失的稳定的、双连通的涡层,也找到了新的数值解。
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引用次数: 0
Enhanced freestream-preserving finite difference method based on MUSCL for numerical computation of laminar flow 层流数值计算中基于MUSCL的增强保持自由流有限差分法
IF 2.8 3区 工程技术 Q2 MECHANICS Pub Date : 2025-06-13 DOI: 10.1007/s00162-025-00745-1
Tianen Guan, Zijia Huang, Chunguang Xu

The implementation of the finite-difference method in curvilinear coordinates necessitates coordinate transformations, where violations of the Geometric Conservation Law (GCL) lead to loss of freestream preservation. This failure mechanism typically manifests as numerical instability or spurious physical artifacts in simulations. In this paper, we developed a freestream-preserving Monotone Upstream-centered Scheme for Conservation Laws (MUSCL) to solve viscous problems on perturbed grids. The geometrically induced errors are eliminated with the satisfaction of GCL. The central difference method is used for the computation of viscous flux terms, and the least squares method is introduced to enhance the accuracy and robustness of this scheme for solving subsonic viscous problems. The results of several viscous numerical tests demonstrate the reliable freestream-preserving property of the new method compared to MUSCL.

在曲线坐标中实现有限差分法需要进行坐标变换,违反几何守恒定律(GCL)将导致自由流保存的丧失。这种失效机制通常表现为数值不稳定或模拟中的虚假物理伪像。本文提出了一种保持自由流的单调上游中心守恒律格式(MUSCL)来解决扰动网格上的粘性问题。在满足GCL要求的情况下,消除了几何误差。采用中心差分法计算粘性通量项,并引入最小二乘法提高该格式在求解亚音速粘性问题时的精度和鲁棒性。若干粘性数值试验结果表明,与MUSCL相比,新方法具有可靠的自由流保持性能。
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引用次数: 0
A volume-adaptive smoothed particle hydrodynamics (SPH) model for underwater contact explosion 水下接触爆炸的体积自适应光滑粒子流体力学模型
IF 2.2 3区 工程技术 Q2 MECHANICS Pub Date : 2025-05-12 DOI: 10.1007/s00162-025-00744-2
Xiangwei Dong, Chongbo Fu, Feng Zhou, Long Feng, Qiang Zhang

Underwater explosions can generate substantial dynamic loads, leading to damage or failure of solid structures such as submarine pipelines. This process involves the interaction of high-pressure explosion products, water, and solid structures, characterized by transience, multi-phase interaction, and large deformations. In this study, a Lagrange mesh-free method called Smoothed Particle Hydrodynamics (SPH) is employed to establish a fluid-solid interaction (FSI) model for underwater contact explosions. The SPH discrete equations of governing equations of continuum media including fluid and solid are constructed as anti-symmetric forms based on the particle approximation technique and kernel gradient correction scheme. The equation of state is presented to describe the material response in strong interactions for the explosive, water, and solid, respectively. To simulate solid plasticity, the Johnson-Cook constitutive models are integrated into the SPH procedure to capture the behavior of large deformation and damage of metal structures. To address the issue of drastic changes in particle spacing caused by suddenly expanding gas, a modified particle regeneration technique (M-PRT) is proposed to refresh SPH particles in the gas domain according to the volume change rate. The first-order Moving Least Squares (MLS) approach is used to update the variables of refreshed particles, thus the linear variation of field variables is reproduced. The accuracy of the model is verified through several examples, including free-field underwater explosions, near-wall underwater explosions, and underwater contact explosions.

水下爆炸会产生巨大的动载荷,导致海底管道等固体结构的破坏或失效。该过程涉及高压爆炸产物、水和固体结构的相互作用,具有瞬态、多相相互作用和大变形的特点。本文采用拉格朗日无网格光滑粒子流体力学(SPH)方法,建立了水下接触爆炸流固相互作用(FSI)模型。基于粒子近似技术和核梯度校正格式,将流体和固体连续介质控制方程的SPH离散方程构造为反对称形式。给出了描述物质在强相互作用下的状态方程,分别为炸药、水和固体。为了模拟固体塑性,将Johnson-Cook本构模型集成到SPH程序中,以捕捉金属结构的大变形和损伤行为。针对气体突然膨胀导致粒子间距剧烈变化的问题,提出了一种改进的粒子再生技术(M-PRT),根据体积变化率对气域中的SPH粒子进行更新。采用一阶移动最小二乘(MLS)方法对刷新后的粒子进行变量更新,再现了场变量的线性变化。通过自由场水下爆炸、近壁水下爆炸和水下接触爆炸算例验证了模型的准确性。
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引用次数: 0
A note on the similarity between acoustic streaming and gravity wave drift in irrotational fluid motion 关于无旋转流体运动中声流和重力波漂移的相似之处的说明
IF 2.2 3区 工程技术 Q2 MECHANICS Pub Date : 2025-04-15 DOI: 10.1007/s00162-025-00743-3
Jan Erik H. Weber

For inviscid irrotational fluid motion, the nonlinear Lagrangian equations for periodic plane acoustic waves and long gravity waves are formally similar. It then follows that the Stokes drift is similar and can be calculated for the two problems. However, the lack of dissipative processes means that the Eulerian mean current cannot be determined, and hence the acoustic streaming velocity and the Lagrangian mean surface-wave drift remain unknown. To remedy this without altering the irrotational character of the fluid motion, we add a small frictional force which is linear in the velocity, or a so-called Rayleigh friction. Then, the Lagrangian mean drift (Stokes drift (+) Eulerian current) is uniquely determined. With this assumption, the acoustic streaming velocity is (left( gamma +1 right) /2) times the Stokes drift in sound waves, where (gamma ) is the adiabatic constant. For long gravity waves, the Lagrangian mean drift is 3/2 times the Stokes drift in surface waves. These results are valid whatever small the Rayleigh friction coefficient is, as long as it is not zero.

对于无粘无旋流体运动,周期平面声波和长引力波的非线性拉格朗日方程形式相似。由此可见,Stokes漂移是相似的,可以计算出这两个问题。然而,耗散过程的缺乏意味着不能确定欧拉平均电流,因此声流速度和拉格朗日平均表面波漂移仍然未知。为了在不改变流体运动的无旋转特性的情况下弥补这一点,我们增加了一个与速度成线性关系的小摩擦力,即所谓的瑞利摩擦。那么,拉格朗日平均漂移(斯托克斯漂移(+)欧拉电流)是唯一确定的。根据这个假设,声流速度等于(left( gamma +1 right) /2)乘以声波中的斯托克斯漂移,其中(gamma )为绝热常数。对于长引力波,拉格朗日平均漂移是表面波中斯托克斯漂移的3/2倍。这些结果是有效的,无论瑞利摩擦系数是小,只要它不是零。
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引用次数: 0
The effect of obstacle length and height in supercritical free-surface flow 障碍长度和高度对超临界自由表面流动的影响
IF 2.2 3区 工程技术 Q2 MECHANICS Pub Date : 2025-03-12 DOI: 10.1007/s00162-025-00735-3
Hugh Michalski, Trent Mattner, Sanjeeva Balasuriya, Benjamin Binder

Two-dimensional open channel flow past a rectangular disturbance in the channel bottom is considered in the case of supercritical flow, where the dimensionless flow rate is greater than unity. The response of the free surface to the height and length of a rectangular disturbance is investigated using the forced Korteweg–de Vries model of Michalski et al. (Theor Comput Fluid Dyn 38:511–530, 2024). A rich and complex structure of solutions is found as the length of the disturbance increases, especially in the case of a negative disturbance. As the length of the disturbance is decreased, some solutions approach those of the well-studied point forcing approximation, but there are other solutions, for a negative disturbance, that are not predicted by the point forcing model. The stability of steady solutions is then considered numerically with established pseudospectral methods.

在无量纲流速大于1的超临界情况下,考虑了通道底部经过矩形扰动的二维明渠流动。使用Michalski等人的强迫Korteweg-de Vries模型(理论计算流体动力学38:51 - 530,2024)研究了自由表面对矩形扰动高度和长度的响应。随着扰动长度的增加,解的结构丰富而复杂,特别是在负扰动的情况下。随着扰动长度的减小,一些解接近于已得到充分研究的点强迫近似的解,但对于负扰动,还有一些解是点强迫模型无法预测的。然后用已建立的伪谱方法对稳态解的稳定性进行数值计算。
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引用次数: 0
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Theoretical and Computational Fluid Dynamics
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