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Regularized Gaussian 11-moment equations for polyatomic gases: Derivation, linear analysis, and its applications 多原子气体的正则化高斯11矩方程:推导,线性分析及其应用
IF 2.8 3区 工程技术 Q2 MECHANICS Pub Date : 2025-09-08 DOI: 10.1007/s00162-025-00755-z
Anil Kumar, Masrakain Ahmad, Anirudh Singh Rana

This article presents a macroscopic closure for rarefied polyatomic gas flows, focusing on a regularized Gaussian 11-moment (RG11) system. Our model uses a generalized Gaussian distribution-a product of Gaussian and Gamma functions-to capture both translational and internal energies of polyatomic molecules. The closure is achieved through a regularization technique, following Struchtrup & Torrilhon (Physics of Fluids, vol. 15, 2003) approach for R13 equations in monatomic gases. In addition, we use a Bhatnagar-Gross-Krook (BGK)-type relaxation model to evaluate the production terms in the moment equations. The proposed model incorporates three relaxation parameters, which can be tuned to match viscosity, bulk viscosity, and thermal conductivity accurately for the gas under consideration. By applying a Chapman-Enskog-like expansion and an order-of-magnitude analysis, we derive the RG11 equations, featuring non-zero constitutive relations for both internal and translational heat flux. This new formulation is linearly stable in one-dimensional case across all wavelengths and frequencies, aligns well with experimental data for sound wave propagation, and agrees with validated hydrodynamic theories that are known to match experimental results for Rayleigh-Brillouin scattering (RBS), outperforming the Navier-Stokes-Fourier (NSF) equations.

本文提出了稀薄多原子气体流动的宏观闭包,重点研究正则化高斯11矩(RG11)系统。我们的模型使用广义高斯分布——高斯函数和伽马函数的乘积——来捕获多原子分子的平动能和内能。闭合是通过正则化技术实现的,遵循strachtrup & Torrilhon(流体物理学,2003年第15卷)对单原子气体中的R13方程的方法。此外,我们使用BGK (Bhatnagar-Gross-Krook)型松弛模型来评估力矩方程中的产生项。所提出的模型包含三个松弛参数,可以调整以准确匹配所考虑的气体的粘度,体积粘度和导热系数。通过应用Chapman-Enskog-like展开和数量级分析,我们推导出了RG11方程,该方程具有内部和平动热通量的非零本构关系。这个新公式在所有波长和频率的一维情况下都是线性稳定的,与声波传播的实验数据很好地吻合,并且与已知的与瑞利-布里渊散射(RBS)实验结果相匹配的经过验证的流体动力学理论相一致,优于Navier-Stokes-Fourier (NSF)方程。
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引用次数: 0
Implicit immersed boundary method integrated into the Vanka ‘big box’ smoother. 隐式浸入边界法集成到Vanka“大盒子”光滑中。
IF 2.8 3区 工程技术 Q2 MECHANICS Pub Date : 2025-09-08 DOI: 10.1007/s00162-025-00754-0
Kirill Goncharuk, Mukesh Kumar, Oz Oshri, Yuri Feldman

The current study introduces a novel fully coupled monolithic solver for the direct forcing immersed boundary method (IBM) in incompressible flows. The solver simultaneously integrates pressure, velocity, nonlinear convection terms, and Lagrangian forces into a unified framework, leveraging a modified big-box Vanka smoother extended with additional Lagrange multipliers arising from the IBM formulation. Central to the approach is the use of a Schur complement decomposition, which reduces the operator size by two-thirds while preserving both stability and accuracy. The solver’s monolithic structure eliminates splitting errors and artificial pressure boundary conditions, common drawbacks of segregated methods. Additionally, the developed methodology enables high CFL numbers (up to 0.5), making it particularly effective for moving boundary simulations. Verification studies cover a broad set of benchmark problems, including both stationary and moving immersed bodies across a wide range of Reynolds numbers. These tests confirm that the solver achieves computational times comparable to existing semi-implicit methods while enhancing accuracy and stability. By addressing key challenges in high-fidelity incompressible flow simulations, the proposed method offers a robust and broadly applicable monolithic solver.

针对不可压缩流的直接强迫浸入边界法(IBM),提出了一种新的全耦合单片求解器。求解器同时将压力、速度、非线性对流项和拉格朗日力集成到一个统一的框架中,利用改进的大盒Vanka平滑器,扩展了来自IBM公式的附加拉格朗日乘子。该方法的核心是使用Schur补分解,它将算子的大小减少了三分之二,同时保持了稳定性和准确性。求解器的整体结构消除了分离方法的常见缺陷——分裂误差和人为压力边界条件。此外,开发的方法可以实现高CFL数(高达0.5),使其对移动边界模拟特别有效。验证研究涵盖了广泛的基准问题,包括在广泛的雷诺数范围内的静止和移动浸入体。这些测试证实,求解器在提高精度和稳定性的同时,实现了与现有半隐式方法相当的计算时间。通过解决高保真不可压缩流动模拟中的关键挑战,该方法提供了一个鲁棒且广泛适用的单片求解器。
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引用次数: 0
Peristaltic Eyring-Powell Nanofluid Flow Linking with Microorganisms across a Curved Channel 蠕动埃林-鲍威尔纳米流体流动与微生物通过弯曲通道连接
IF 2.8 3区 工程技术 Q2 MECHANICS Pub Date : 2025-08-29 DOI: 10.1007/s00162-025-00751-3
Mona A. A. Mohamed

The study of peristaltic Eyring-Powell nanofluid (EPF) with microorganisms is crucial in biomedical and industrial processes, improving drug delivery systems, bioreactors, and targeted microorganism transport. The EPF in a curved peristaltic channel under the influence of a uniform normal magnetic field (MF) and inside a permeable material is therefore considered in the current issue. The flow also comprises microorganisms and is motivated by the effects of porous media, Joule heating, non-Newtonian dissipation, and chemical reactions. The current work innovation stems from the inclusion of nanoparticles and microorganisms through non-Newtonian fluid flows in a curved channel, utilizing the curvilinear coordinates, which have several implications in engineering, industry, and biology. The flow under contemplation is caused by peristaltic waves that have a constant wavelength and amplitude. The problem’s governing equations are modeled using curvilinear coordinates. The goal is to maintain simplicity, and subsequently, so the problem is illustrated in the wave frame instead of the fixed frame. Under low Reynolds number and long wavelength approximation in the wave frame of reference, the mathematical framework addresses energy, momentum, nanomaterial’s volume fraction, and microbe concentration together with appropriate boundary conditions (BCs). The solutions of the governing system are handled with the help of shooting criteria and an appropriate numerical implicit method via the fourth-order Runge-Kutta (RK-4). The physical outcomes concerning flow parameters are presented to indicate the enhancement and decay factors of all relevant distributions, together with the heat and mass transfer coefficients. It is found that the factors that enhance the existence of nanoparticles and heat broadcast are the same that decay the presence of microbes, which gives practical importance to the current issue.

具有微生物的蠕动型埃林-鲍威尔纳米流体(EPF)的研究在生物医学和工业过程中至关重要,可以改善药物输送系统、生物反应器和靶向微生物运输。因此,本课题考虑了均匀法向磁场作用下弯曲蠕动通道内和可渗透材料内部的EPF。流动还包括微生物,并受到多孔介质、焦耳加热、非牛顿耗散和化学反应的影响。当前的工作创新源于纳米颗粒和微生物通过非牛顿流体在弯曲通道中流动,利用曲线坐标,这在工程、工业和生物学中具有许多意义。所观察到的流动是由具有恒定波长和振幅的蠕动波引起的。该问题的控制方程采用曲线坐标建模。我们的目标是保持简单,因此,问题在波动框架中而不是固定框架中得到说明。在低雷诺数和长波长近似的波参照系下,数学框架处理能量、动量、纳米材料体积分数和微生物浓度以及适当的边界条件(bc)。通过四阶龙格-库塔(RK-4),利用射击准则和适当的数值隐式方法对控制系统的解进行了处理。给出了有关流动参数的物理结果,以表明所有相关分布的增强和衰减因子,以及传热和传质系数。研究发现,提高纳米粒子存在和热传播的因素与降低微生物存在的因素是相同的,这对当前的问题具有重要的现实意义。
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引用次数: 0
Channel Flow with an Ice Constriction: Direct Simulation and Reduced-System Analysis 冰收缩的河道流动:直接模拟和简化系统分析
IF 2.8 3区 工程技术 Q2 MECHANICS Pub Date : 2025-08-29 DOI: 10.1007/s00162-025-00753-1
Reza T. Batley, Frank T. Smith

The study here is of two-dimensional constricted channel flows and insight into their properties as the degree of constriction varies. This is potentially helpful for a range of applications as well as being of basic scientific interest. Two main computational approaches are taken, one via direct numerical simulation of the Navier-Stokes equations, and the other in the large Reynolds number limit where the boundary layer equations apply wall-to-wall. The focus is on understanding more of, and quantifying, the relatively unknown effects of wall icing in channel flow of water, as well as making quantitative comparisons between solutions from the two computational approaches and similar comparisons with recent work on the melting of wall-mounted ice. Flow separation, eddy lengths, pressure responses for sufficiently constricted internal vessels and upstream or downstream influence are examined. The retention of the ice when undercooling is present at the vessel wall is also studied. Severe blocking followed by eventual mild blocking or complete unblocking of the water flow is commonly found.

这里的研究是二维狭窄的河道流动,并深入了解其性质随着收缩程度的变化。这对一系列应用有潜在的帮助,并且具有基本的科学兴趣。采用了两种主要的计算方法,一种是通过直接数值模拟Navier-Stokes方程,另一种是在大雷诺数极限下,边界层方程应用于壁面到壁面。重点是更多地了解和量化渠道水流中壁冰相对未知的影响,以及对两种计算方法的解决方案进行定量比较,并与最近关于壁上冰融化的工作进行类似比较。流动分离,涡流长度,压力响应充分收缩的内部容器和上游或下游的影响进行了检查。还研究了容器壁过冷时冰的滞留。通常会出现严重堵塞,然后是最终的轻度堵塞或水流完全畅通。
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引用次数: 0
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
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Theoretical and Computational Fluid Dynamics
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