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GPU parallel implementation of a finite volume lattice Boltzmann method for incompressible flows 针对不可压缩流动的有限体积晶格玻尔兹曼方法的 GPU 并行执行
IF 2.5 3区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS Pub Date : 2024-10-26 DOI: 10.1016/j.compfluid.2024.106460
Mengke Wen , Siyuan Shen , Weidong Li
This work presents a graphics processing units (GPU) parallel algorithm of a cell-centered finite volume lattice Boltzmann method (FVLBM) on unstructured meshes. In the present GPU parallel algorithm, the parallelization is performed in the physical space. To reduce the frequency of GPU memory accesses, this algorithm develops coalesced access to GPU memory. In addition, to avoid the race for resources leading to data anomalies, such as dirty read or phantom read etc., and the double counting for flux calculation, the efficient face-based data structure often used for flux calculation in cells in the central processing unit (CPU) version of FVLBM is modified into a face-based data structure used for the fluxes on all faces, followed by a cell-based loop for the final residuals in all cells. Therefore, the proposed GPU parallel algorithm does not need to use the resource lock and retains the high efficiency of the face-based data structure in the fluxes computation to enhance its’ parallel efficiency. Additionally, to demonstrate the computational efficiency of the proposed GPU parallel algorithm, various benchmark studies are performed in this work by the proposed parallel scheme on a double precision NVIDIA GeForce RTX 3090Ti GPU card, including (a) the lid-driven flow in a two-dimensional (2D) square cavity, (b) a 2D flow past a cylinder, and (c) the lid-driven flow in a three-dimensional (3D) cubic cavity. The numerical results show that the proposed GPU parallel algorithm can be as accurate as the original CPU serial scheme with 1 to 2 orders of speedup.
本研究提出了一种在非结构网格上以单元为中心的有限体积晶格玻尔兹曼法(FVLBM)的图形处理器(GPU)并行算法。在本 GPU 并行算法中,并行化是在物理空间中进行的。为了降低 GPU 内存访问频率,该算法开发了对 GPU 内存的聚合访问。此外,为了避免资源争夺导致数据异常(如脏读或幻读等)以及流量计算的重复计算,FVLBM 的中央处理器(CPU)版本中通常用于单元流量计算的基于面的高效数据结构被修改为基于面的数据结构,用于计算所有面上的流量,然后通过基于单元的循环来计算所有单元的最终残差。因此,所提出的 GPU 并行算法无需使用资源锁,并在通量计算中保留了基于面的数据结构的高效率,从而提高了并行效率。此外,为了证明所提出的GPU并行算法的计算效率,本研究利用所提出的并行方案在双精度NVIDIA GeForce RTX 3090Ti GPU卡上进行了各种基准研究,包括(a)二维(2D)方形空腔中的顶盖驱动流动,(b)经过圆柱体的二维流动,以及(c)三维(3D)立方体空腔中的顶盖驱动流动。数值结果表明,所提出的 GPU 并行算法与原来的 CPU 串行方案一样精确,而且速度提高了 1 到 2 个数量级。
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引用次数: 0
Symmetry-preserving discretizations in Lagrangian cell-centered hydrodynamics 拉格朗日细胞中心流体力学中的对称保留离散化
IF 2.5 3区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS Pub Date : 2024-10-24 DOI: 10.1016/j.compfluid.2024.106462
Xihua Xu
This paper discusses constructing discretizations in Lagrangian cell-centered hydrodynamics (CCH) that preserve cylindrical symmetry on unequal-angle-zoned grids in two-dimensional Cartesian geometry. We achieve this by modifying the nodal solver (Corot and Mercier, 2018) and updating the total and internal energy equations. The method is a unique solution to the challenging problem of ensuring symmetry in vectors. A criterion is established for determining whether or not this symmetry correction should be applied. We prove that both nodal and zonal quantities maintain a symmetry distribution. Numerical illustrations using unequal-angle initial zoning are presented to demonstrate the efficiency of the scheme.
本文讨论了在二维笛卡尔几何的不等角分区网格上构建拉格朗日细胞中心流体力学(CCH)离散化,以保持圆柱对称性。我们通过修改节点求解器(Corot 和 Mercier,2018 年)和更新总能量和内能方程来实现这一目标。该方法是确保矢量对称性这一难题的独特解决方案。我们建立了一个标准,用于确定是否应用这种对称性修正。我们证明了节点量和带状量都保持了对称分布。使用不等角初始分区进行了数值说明,以展示该方案的效率。
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引用次数: 0
A coupled immersed boundary method and wall modelling framework for high-Reynolds number flows over complex terrain 复杂地形上高雷诺数流动的沉浸边界法与壁面建模耦合框架
IF 2.5 3区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS Pub Date : 2024-10-23 DOI: 10.1016/j.compfluid.2024.106457
Jay A. Patel , Ankita Maity , Niranjan S. Ghaisas
We present the development and validation of an immersed boundary method (IBM) along with a wall model (WM) to simulate atmospheric boundary-layer flows over complex terrain. The framework presented here has two novel aspects over standard IBM implementations. First, the underlying schemes are global in nature and require specification of values throughout the solid region. Second, to enable high-Reynolds number simulations, a wall model is coupled to the IBM. The proposed numerical framework is shown to have second-order accuracy. The framework is validated by simulating flow over a 2D as well as 3D cosine-squared hill and comparing to previously published experimental results. The mean velocity and turbulence intensity are reproduced accurately by our LES. The flow over the Bolund hill, marked by steep slopes which makes this a challenging test case, is also simulated and results are compared to field observations showing good agreement. The framework also accurately reproduces the turbulent statistics in the wake of a turbine situated on a flat terrain, with the flat terrain modelled using the IBWM framework, thus demonstrating its applicability to high-Reynolds number atmospheric and wind farm flows over complex terrain.
我们介绍了沉浸边界法(IBM)和壁面模型(WM)的开发和验证情况,以模拟复杂地形上的大气边界层流动。与标准的 IBM 实现相比,这里介绍的框架有两个新颖之处。首先,基础方案是全局性的,需要指定整个固体区域的数值。其次,为实现高雷诺数模拟,壁面模型与 IBM 相耦合。研究表明,所提出的数值框架具有二阶精度。通过模拟二维和三维余弦平方山的流动,并与之前公布的实验结果进行比较,验证了该框架的有效性。我们的 LES 准确地再现了平均速度和湍流强度。博伦德山丘上有陡峭的斜坡,这使其成为一个具有挑战性的测试案例,我们也模拟了博伦德山丘上的气流,并将结果与现场观测结果进行了比较,结果显示两者吻合良好。该框架还精确再现了位于平坦地形上的涡轮机尾流中的湍流统计数据,平坦地形使用 IBWM 框架进行建模,从而证明了该框架适用于复杂地形上的高雷诺数大气和风电场气流。
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引用次数: 0
Resolving subgrid-scale structures for multiphase flows using a filament moment-of-fluid method 利用丝状流体力矩法解析多相流的亚网格尺度结构
IF 2.5 3区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS Pub Date : 2024-10-22 DOI: 10.1016/j.compfluid.2024.106455
Philippe Hergibo , Timothy N. Phillips , Zhihua Xie
Multiphase flows are present in many industrial and engineering applications as well as in some physical phenomena. Capturing the interface between the phases for complex flows is challenging and requires an accurate method, especially to resolve fine-scale structures. The moment-of-fluid (MOF) method improves drastically the accuracy of interface reconstruction compared to previous geometrical methods. Instead of refining the mesh to capture increased levels of detail, the MOF method, which uses zeroth and first moments as well as a conglomeration algorithm, enables subgrid structures such as filaments to be captured at a small extra cost. Coupled to a finite volume Navier–Stokes solver, the MOF method has been tested on a fixed grid and validated using well-known benchmark problems such as dam break flows, the Rayleigh–Taylor and Kelvin–Helmholtz instability problems, and a rising bubble. The ability of the novel filament MOF method to capture the filamentary structures that eventually form for the Rayleigh–Taylor instability and rising bubble problems is assessed. Good agreement has been found with other numerical results and experimental measurements available in the literature.
多相流存在于许多工业和工程应用以及某些物理现象中。捕捉复杂流动中各相间的界面具有挑战性,需要一种精确的方法,尤其是解决细尺度结构的方法。与以前的几何方法相比,流体动量(MOF)方法大大提高了界面重建的精确度。MOF 方法使用零矩和一阶矩以及聚合算法,无需细化网格来捕捉更多细节,只需少量额外成本就能捕捉到细丝等亚网格结构。MOF 方法与有限体积纳维-斯托克斯求解器耦合,已在固定网格上进行了测试,并使用著名的基准问题进行了验证,如水坝断流、瑞利-泰勒和开尔文-赫尔姆霍兹不稳定性问题以及上升气泡。评估了新型丝状 MOF 方法捕捉雷利-泰勒不稳定性和上升气泡问题最终形成的丝状结构的能力。研究发现,该方法与其他数值结果和文献中的实验测量结果具有良好的一致性。
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引用次数: 0
An evaluation of the hybrid Fokker–Planck-DSMC approach for high-speed rarefied gas flows 高速稀薄气体流的福克-普朗克-DSMC 混合方法评估
IF 2.5 3区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS Pub Date : 2024-10-22 DOI: 10.1016/j.compfluid.2024.106456
Sanghun Kim, Eunji Jun
The Direct Simulation Monte Carlo (DSMC) method has been widely used for simulations of rarefied gas flows. It has been proven that the numerical solution of the DSMC method converges to the Boltzmann equation, providing a solid physical foundation for high Knudsen numbers. However, many aerospace engineering problems include both low and high-density regions in a single domain, making the DSMC method computationally expensive. Over the past decade, the particle Fokker–Planck (FP) method has been studied as a means to reduce computational costs near the continuum regime. While enhancing efficiency, the FP method loses physical accuracy at high Knudsen numbers. Aiming for universal accuracy and efficiency across the whole range of Knudsen numbers, the hybrid FP-DSMC method has been studied. Nevertheless, consistent comparisons among the DSMC, FP, and hybrid FP-DSMC methods have received limited attention so far. This paper presents a consistent comparative study of the DSMC, FP, and hybrid FP-DSMC methods to assess the accuracy and efficiency of the hybrid FP-DSMC method. The hybrid FP-DSMC solver is developed based on the open-source SPARTA framework. The benchmark problems include supersonic flow in a planar nozzle, hypersonic flow around a cylinder, and hypersonic flow around a THAAD-like missile. The results demonstrate that the hybrid FP-DSMC method can be more efficient than the DSMC method while being more accurate than the FP method. The speed-up achieved by the FP-DSMC method ranged from 1.5 to 14 times compared to the converged DSMC simulation.
直接模拟蒙特卡罗(DSMC)方法已被广泛用于稀薄气体流动的模拟。实践证明,DSMC 方法的数值解收敛于玻尔兹曼方程,为高努森数提供了坚实的物理基础。然而,许多航空航天工程问题包括单个域中的低密度和高密度区域,这使得 DSMC 方法的计算成本非常昂贵。在过去的十年中,粒子福克-普朗克(FP)方法一直被作为一种降低连续系统计算成本的方法来研究。在提高效率的同时,FP 方法在高 Knudsen 数时失去了物理精度。为了在整个 Knudsen 数范围内实现普遍的精度和效率,人们研究了 FP-DSMC 混合方法。然而,迄今为止,DSMC、FP 和 FP-DSMC 混合方法之间的一致性比较受到的关注还很有限。本文对 DSMC、FP 和混合 FP-DSMC 方法进行了一致的比较研究,以评估混合 FP-DSMC 方法的准确性和效率。混合 FP-DSMC 求解器是基于开源 SPARTA 框架开发的。基准问题包括平面喷嘴中的超音速流动、围绕圆柱体的高超声速流动以及围绕类似于 THAAD 导弹的高超声速流动。结果表明,FP-DSMC 混合方法比 DSMC 方法更高效,同时比 FP 方法更精确。与收敛后的 DSMC 仿真相比,FP-DSMC 方法的速度提高了 1.5 到 14 倍。
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引用次数: 0
An improved pressure gradient method for viscous incompressible flows 粘性不可压缩流的改进压力梯度法
IF 2.5 3区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS Pub Date : 2024-10-22 DOI: 10.1016/j.compfluid.2024.106448
Zhisong Li , Ye Li
The pressure gradient method solves the viscous incompressible flow with the pressure gradients, rather than the pressure, as unknown variables. Two variants of the pressure gradient method have been developed in the past but have not received much attention due to their unsatisfactory performance or implementation complexity. Based on the artificial compressibility concept, this study proposes an improved pressure gradient method. One distinct feature of this method is that it requires no pressure/pressure gradient boundary condition or special treatment on wall boundaries. An auxiliary variable is introduced to represent the velocity dilatation, greatly simplifying the spatial discretization and computational procedure. The mathematical formulations are elaborated and compared with the previous pressure gradient methods, followed by discussions of compatibility relationships, boundary condition setup, and an extension to a pressure Poisson-like equation. Four validation examples are performed for various flow scenarios, and the solutions and domain solenoidity are examined for each case. The study also compares associated computational methods, different pressure boundary conditions, and flow characteristics, demonstrating the benefits of the present method.
压力梯度法以压力梯度而非压力作为未知变量来求解粘性不可压缩流动。压力梯度法的两个变体在过去已被开发出来,但由于其性能不理想或实施复杂,并未受到广泛关注。基于人工可压缩性概念,本研究提出了一种改进的压力梯度法。该方法的一个显著特点是不需要压力/压力梯度边界条件,也不需要对壁面边界进行特殊处理。引入了一个辅助变量来表示速度扩张,从而大大简化了空间离散和计算过程。详细阐述了数学公式,并与之前的压力梯度方法进行了比较,随后讨论了兼容性关系、边界条件设置以及压力泊松方程的扩展。针对不同的流动情况进行了四次验证,并检查了每种情况下的解决方案和域电磁性。研究还比较了相关的计算方法、不同的压力边界条件和流动特性,展示了本方法的优势。
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引用次数: 0
Boundary conditions for SPH through energy conservation 通过能量守恒实现 SPH 的边界条件
IF 2.5 3区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS Pub Date : 2024-10-18 DOI: 10.1016/j.compfluid.2024.106454
Jose Luis Cercos-Pita , Daniel Duque , Pablo Eleazar Merino-Alonso , Javier Calderon-Sanchez
Dealing with boundary conditions in Smoothed Particle Hydrodynamics (SPH) poses significant difficulties, indeed being one of the SPHERIC Grand Challenges. In particular, wall boundary conditions have been pivotal in SPH model development since it evolved from astrophysics to more generic fluid dynamics simulations. Despite considerable attention from researchers and numerous publications dedicated to formulating and assessing wall boundary conditions, few of them have addressed the crucial aspect of energy conservation. This work introduces a novel boundary condition designed with energy conservation as a primary consideration, effectively extending the unconditional stability of SPH to problems involving wall boundary conditions. The result is formulated within the framework of the Boundary Integrals technique. The proposal is tested on a number of cases: normal impact against a wall, adiabatic oscillations of a piston, dam break, and the water landing of a spacecraft.
处理平滑粒子流体力学(SPH)中的边界条件是一个重大难题,实际上也是 SPHERIC 大挑战之一。特别是,自从平滑粒子流体力学(SPH)从天体物理学发展到更通用的流体动力学模拟以来,壁面边界条件一直是 SPH 模型发展的关键。尽管研究人员对制定和评估壁边界条件给予了极大关注,并发表了大量相关论文,但很少有论文涉及能量守恒这一关键问题。这项研究引入了一种以能量守恒为主要考虑因素的新型边界条件,有效地将 SPH 的无条件稳定性扩展到涉及壁边界条件的问题。这一结果是在边界积分技术的框架内提出的。该提议在多种情况下进行了测试:对墙壁的正常撞击、活塞的绝热振荡、水坝破裂以及航天器的水上着陆。
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引用次数: 0
Effects of two-dimensional reed oscillation on airflow and sound generation in a single-reed instrument 二维哨片振荡对单簧乐器气流和发声的影响
IF 2.5 3区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS Pub Date : 2024-10-17 DOI: 10.1016/j.compfluid.2024.106452
Tsukasa Yoshinaga , Reo Baba , Hiroshi Yokoyama , Tetsuro Shoji , Akira Miki , Akiyoshi Iida
While two-dimensional (2D) reed oscillation modes of single-reed woodwind instruments have been reported in previous studies, little is known about their effects on airflow and sound generation. In this study, we conducted aeroacoustic simulations of a clarinet mouthpiece and resonator coupled with one-dimensional (1D) and 2D reed deformation models and investigated the changes in flow and sound generation due to the 2D reed vibration. The 1D and 2D reeds were modeled using 1D beam and thin plate theories, respectively, whereas the three-dimensional airflow was simulated by solving the compressible Navier–Stokes equations. The self-sustained oscillations of the 2D reed model mainly exhibited a flexural mode at the fundamental frequency, which is consistent with previous observations. Complex torsional modes were observed only at higher harmonic frequencies. A comparison between the 1D and 2D reed models demonstrated that the 2D reed opened later at the side face of the mouthpiece than the 1D reed owing to the torsional mode, which changed the time variation of the flow rate into the mouthpiece and the far-field sound in the high-frequency range. These results suggest the importance of the torsional deformation characteristics of reeds on the timbre of single-reed instruments.
尽管之前的研究已经报道了单簧木管乐器的二维(2D)哨片振荡模式,但对其对气流和发声的影响却知之甚少。在这项研究中,我们对单簧管吹嘴和共鸣器进行了气动声学模拟,并结合一维(1D)和二维簧片变形模型,研究了二维簧片振动对气流和声音产生的影响。一维和二维簧片分别使用一维梁和薄板理论建模,而三维气流则通过求解可压缩纳维-斯托克斯方程进行模拟。二维苇片模型的自持振荡主要表现为基频处的挠曲模式,这与之前的观察结果一致。只有在较高的谐波频率下才能观察到复杂的扭转模式。一维和二维哨片模型之间的比较表明,二维哨片在吹嘴侧面的打开时间晚于一维哨片,原因是扭转模式改变了吹嘴流量的时间变化和高频范围内的远场声。这些结果表明,哨片的扭转变形特性对单簧乐器的音色具有重要影响。
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引用次数: 0
Momentum exchange method for quantum Boltzmann methods 量子波尔兹曼方法的动量交换法
IF 2.5 3区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS Pub Date : 2024-10-16 DOI: 10.1016/j.compfluid.2024.106453
Merel A. Schalkers, Matthias Möller
The past years have seen a surge in quantum algorithms for computational fluid dynamics (CFD). These algorithms have in common that whilst promising a speed-up in the performance of the algorithm, no specific method of measurement has been suggested. This means that while the algorithms presented in the literature may be promising methods for creating the quantum state that represents the final flow field, an efficient measurement strategy is not available. This paper marks the first quantum method proposed to efficiently calculate quantities of interest (QoIs) from a state vector representing the flow field. In particular, we propose a method to calculate the force acting on an object immersed in the fluid using a quantum version of the momentum exchange method (MEM) that is commonly used in lattice Boltzmann methods to determine the drag and lift coefficients. In order to achieve this we furthermore give a scheme that implements bounce back boundary conditions on a quantum computer, as those are the boundary conditions the momentum exchange method is designed for.
过去几年中,计算流体动力学(CFD)的量子算法激增。这些算法的共同点是,虽然有望加快算法性能,但没有提出具体的测量方法。这意味着,虽然文献中介绍的算法可能是创建代表最终流场的量子态的有前途的方法,但却没有有效的测量策略。本文首次提出了一种量子方法,可从代表流场的状态矢量中有效计算出感兴趣的量子量(QoIs)。特别是,我们提出了一种使用量子版动量交换法(MEM)计算浸入流体中物体所受作用力的方法,该方法常用于确定阻力和升力系数的晶格玻尔兹曼方法。为了实现这一目标,我们进一步给出了一种在量子计算机上实现反弹边界条件的方案,因为这些正是动量交换法设计的边界条件。
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引用次数: 0
A numerical method for simulating variable density flows in membrane desalination systems 模拟膜脱盐系统中变密度流动的数值方法
IF 2.5 3区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS Pub Date : 2024-10-11 DOI: 10.1016/j.compfluid.2024.106449
Federico Municchi , Yiming Liu , Jingbo Wang , Tzahi Y. Cath , Craig S. Turchi , Michael B. Heeley , Eric M.V. Hoek , David Jassby , Nils Tilton
We present a novel method for simulating unsteady, variable density, fluid flows in membrane desalination systems. By assuming the density varies only with concentration and temperature, the scheme decouples the solution of the governing equations into two sequential blocks. The first solves the governing equations for the temperature and concentration fields, which are used to compute all thermophysical properties. The second block solves the conservation of mass and momentum equations for the velocity and pressure. We show that this is computationally more efficient than schemes that iterate over the full coupled equations in one block. We verify that the method achieves second-order spatial–temporal accuracy, and we use the method to investigate buoyancy-driven convection in a desalination process called vacuum membrane distillation. Specifically, we show that with gravity properly oriented, variations in temperature and concentration can trigger a double-diffusive instability that enhances mixing and improves water recovery. We also show that the instability can be strengthened by providing external heating.
我们提出了一种新方法,用于模拟膜脱盐系统中的非稳态、变密度流体流动。通过假设密度仅随浓度和温度变化,该方案将调节方程的求解分解为两个连续的模块。第一块求解温度场和浓度场的控制方程,用于计算所有热物理特性。第二个区块求解速度和压力的质量和动量守恒方程。我们证明,与在一个区块中遍历全部耦合方程的方案相比,这种方法的计算效率更高。我们验证了该方法达到了二阶时空精度,并使用该方法研究了真空膜蒸馏海水淡化过程中的浮力驱动对流。具体来说,我们表明,在重力方向正确的情况下,温度和浓度的变化会引发双扩散不稳定性,从而加强混合并提高水回收率。我们还表明,通过提供外部加热可以加强这种不稳定性。
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引用次数: 0
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