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Journal of Turbulence最新文献

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Spectral energy transfer analysis of a forced homogeneous isotropic turbulence using triple decomposition of velocity gradient tensor 利用速度梯度张量的三重分解对强制均质各向同性湍流进行谱能传递分析
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-03-22 DOI: 10.1080/14685248.2024.2332318
Mani Fathali, Saber Khoei
Triple decomposition of the velocity gradient tensor is exploited to investigate the role of the simple-shear, normal-strain, and rigid-body rotation, in the turbulent kinetic energy transfer of a ...
利用速度梯度张量的三重分解来研究简单剪切、法向应变和刚体旋转在湍流动能传递中的作用。
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引用次数: 0
Multi-spatial scale and multi-frequency resolution Proper Orthogonal Decomposition for patterns of wall-streamwise pressure gradient fluctuation of impinging jets 多空间尺度和多频率分辨率的适当正交分解,用于分析撞击喷流的壁流压力梯度波动模式
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-03-20 DOI: 10.1080/14685248.2024.2330056
Miaoxin Han, Yonghua You
In the coating industry, seemingly ordered millimeter-scale W or X-like patterns inevitably appear on the coating wiped by jets. Considering the dynamic control of coating thickness by the maximum ...
在喷涂工业中,喷射器擦拭的涂层上不可避免地会出现看似有序的毫米级 W 或 X 形图案。考虑到通过最大喷射量对涂层厚度进行动态控制的问题,我们需要对喷嘴进行改进。
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引用次数: 0
Effects of axial distance on flow behaviours of continuous jet impinging on a flat surface using a finite confined nozzle 轴向距离对使用有限约束喷嘴冲击平面的连续射流流动行为的影响
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-03-19 DOI: 10.1080/14685248.2024.2330065
Siva Ramalingam, Minh Duc Le, Ching Min Hsu
The velocity fields and impinging pressure characteristics of confined jet impinges on a flat surface subject to the influence of various axial stages of a flat plate were experimentally examined. ...
实验研究了受平板不同轴向级数影响的平面上密闭射流撞击的速度场和撞击压力特性。...
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引用次数: 0
Laminar to turbulent transitions of pipe flows by resonances of natural frequencies of components of test sections 通过试验段各部分固有频率的共振实现管道流从层流到湍流的过渡
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-02-22 DOI: 10.1080/14685248.2024.2319066
F. Durst, G. Biswas, K. Haddad
This investigation analyses special papers and doctoral theses that treat transitions of pipe flows as a resonance phenomenon of wave frequencies. These frequencies are natural frequencies of pipe ...
本研究分析了将管道流动的转变视为波频共振现象的专题论文和博士论文。这些频率是管道的自然频率 ...
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引用次数: 0
Quantifying instantaneous flow reversal of tracer particles in subsonic, transonic and supersonic flows past a circular cylinder 亚音速、跨音速和超音速流经圆筒时示踪粒子瞬时流动逆转的定量分析
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-01-11 DOI: 10.1080/14685248.2023.2293700
Huiying Zhang, James M. Wallace, Xiaohua Wu
Tracer pathline statistics have rarely, if at all, been used in the investigation of compressible subsonic, transonic and supersonic flows past a circular cylinder. Here, we report pathline histogr...
在研究经过圆柱体的可压缩亚音速、跨音速和超音速流动时,很少使用示踪路径线统计。在这里,我们报告了路径线直方图。
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引用次数: 0
Exciting turbulence in an elongated domain 拉长域中的激波湍流
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-01-08 DOI: 10.1080/14685248.2023.2298882
Tong Wu, Le Fang, Joachim Peinke, Wouter J. T. Bos
Motivated by recent experimental results in grid turbulence with very long streamwise velocity correlations, we consider numerical simulations of turbulence in a domain that is elongated in one dir...
受最近在具有极长流向速度相关性的网格湍流中取得的实验结果的启发,我们考虑了在沿一个方向拉长的域中对湍流进行数值模拟的问题。
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引用次数: 0
Evaluating anisotropic minimum dissipation, sigma and modulated gradient subgrid-scale models in large-eddy simulation of compressible mixing layers 评估可压缩混合层大涡流模拟中的各向异性最小耗散、σ和调制梯度子网格尺度模型
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2023-12-25 DOI: 10.1080/14685248.2023.2297901
Peddamma Vishwaja, Niranjan S. Ghaisas
We evaluate three subgrid-scale (SGS) models in large eddy simulations (LES) of compressible mixing layers up to convective Mach number (Mc) 2.0. The initial momentum-thickness based Reynolds numbe...
我们评估了对流马赫数(Mc)2.0 以下可压缩混合层大涡度模拟(LES)中的三种子网格尺度(SGS)模型。以初始动量厚度为基础的雷诺数...
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引用次数: 0
Circulation in turbulent flow through a contraction 湍流在收缩处的循环
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2023-12-20 DOI: 10.1080/14685248.2023.2284187
Vivek Mugundhan, Sigurdur T. Thoroddsen
We study experimentally the statistical properties and evolution of circulation in a turbulent flow passing through a smooth 2-D contraction. The turbulence is generated with active grids to reach ...
我们通过实验研究了通过平滑二维收缩的湍流中环流的统计特性和演变。湍流是通过主动网格生成的,以达到...
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引用次数: 0
Advanced detached-eddy simulation of the MD 30P-30N three-element airfoil MD 30P-30N三元翼型的先进分离涡模拟
4区 工程技术 Q3 MECHANICS Pub Date : 2023-11-05 DOI: 10.1080/14685248.2023.2278506
Mikhail Shur, Mikhail Strelets, Philippe Spalart, Andrey Travin
AbstractAn experimental version in the Detached-Eddy Simulation (DES) family (called Advanced DES or ADES) is introduced and tested on a geometry that is fairly complex but two-dimensional. The essential change in ADES is that the user is given control of the regions treated with full turbulence modelling (RANS) and those treated with Large-Eddy Simulation (LES). This zonal character makes the approach more powerful, but less practical, so that in its current state it is not ready for industrial CFD. The grid requirements of the two regions are very different, and multi-block grid structure is natural. Another key feature is a Volumetric Synthetic Turbulence Generator (VSTG), installed to feed the LES region with viable resolved turbulence, so that the resolved Reynolds stresses rapidly substitute for the modelled Reynolds stresses present in the RANS region. The VSTG operates in a volume, rather than on a surface and can be active in attached boundary layers, at a trailing edge, or after separation. The well-known McDonnell-Douglas 30P-30N airfoil is simulated with periodic lateral boundary conditions. The VSTG is successful, and the desired nature of simulation is obtained in each region. ADES involves zonal decisions, but appears robust. An inertial range is clearly indicated in frequency spectra. A grid-refinement study is included, as well as variations in lateral domain size and STG positions; this led to a matrix of 11 simulations. Cases are shown at four angles of attack and with three RANS models in addition to ADES. Pressure and friction distributions and velocity and shear stress profiles are compared in detail. The prospects for an evolution of ADES into a practical routine approach in the long term are discussed.KEYWORDS: Advanced detached-eddy simulationmulti-element wings3-element High-lift airfoils AcknowledgementsAll the computations were conducted with the use of the HP computing facilities of the Peter the Great Saint-Petersburg Polytechnic University (http://www.spbstu.ru; accessed on August 24 2023) within the framework of the scientific program of the National Center for Physics and Mathematics, section #2 ‘Mathematical modeling on Zetta-scale and Exa-scale Supercomputers. Stage 2023-2025’.Disclosure statementNo potential conflict of interest was reported by the author(s).Additional informationFundingThis work was supported by Ministry of Science and Higher Education of the Russian Federation: [Grant Number 075-15-2022-311].
摘要介绍了分离涡模拟(DES)系列中的一个实验版本(称为高级DES或ADES),并在相当复杂的二维几何结构上进行了测试。ADES的本质变化是,用户可以控制用全湍流模型(RANS)处理的区域和用大涡模拟(LES)处理的区域。这种区域性特征使得该方法更强大,但实用性较差,因此在目前的状态下,它还不适合工业CFD。两个区域的网格要求差别很大,多块网格结构是自然的。另一个关键特性是体积合成湍流发生器(VSTG),安装后可向LES区域提供可行的已解湍流,因此已解的雷诺应力可迅速替代RANS区域中模拟的雷诺应力。VSTG在一个体积内工作,而不是在一个表面上工作,可以在附着的边界层、尾缘或分离后工作。著名的麦克唐纳-道格拉斯30P-30N翼型是模拟周期性横向边界条件。VSTG是成功的,并且在每个区域都获得了期望的仿真性质。ADES涉及区域决策,但看起来很稳健。惯性范围在频谱中清楚地表示出来。包括网格细化研究,以及横向域大小和STG位置的变化;这导致了一个包含11个模拟的矩阵。病例显示为四个攻角,除ADES外还有三种RANS模型。详细比较了压力和摩擦分布、速度和剪应力分布。讨论了从长远来看,ADES发展成为一种实用的常规方法的前景。关键词:先进分离涡模拟多单元机翼三单元大升力翼型所有计算均使用圣彼得堡彼得大帝理工大学(http://www.spbstu.ru;在国家物理和数学中心的科学计划框架内,第2部分“zeta -scale和Exa-scale超级计算机的数学建模”,于2023年8月24日访问。阶段2023 - 2025年”。披露声明作者未报告潜在的利益冲突。本研究由俄罗斯联邦科学和高等教育部资助:[资助号075-15-2022-311]。
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引用次数: 0
Fractional and tempered fractional models for Reynolds-averaged Navier–Stokes equations reynolds -平均Navier-Stokes方程的分数阶和回火分数阶模型
4区 工程技术 Q3 MECHANICS Pub Date : 2023-10-31 DOI: 10.1080/14685248.2023.2274100
Pavan Pranjivan Mehta
Turbulence is a non-local phenomenon and has multiple-scales. Non-locality can be addressed either implicitly or explicitly. Implicitly, by subsequent resolution of all spatio-temporal scales. However, if directly solved for the temporal or spatially averaged fields, a closure problem arises on account of missing information between two points. To solve the closure problem in Reynolds-averaged Navier-Stokes equations (RANS), an eddy-viscosity hypotheses has been a popular modelling choice, where it follows either a linear or non-linear stress-strain relationship. Here, a non-constant diffusivity is introduced. Such a non-constant diffusivity is also characteristic of non-Fickian diffusion equation addressing anomalous diffusion process. An alternative approach, is a fractional derivative based diffusion equations. Thus, in the paper, we formulate a fractional stress-strain relationship using variable-order Caputo fractional derivative. This provides new opportunities for future modelling effort. We pedagogically study of our model construction, starting from one-sided model and followed by two-sided model. Non-locality at a point is the amalgamation of all the effects, thus we find the two-sided model is physically consistent. Further, our construction can also addresses viscous effects, which is a local process. Thus, our fractional model addresses the amalgamation of local and non-local process. We also show its validity at infinite Reynolds number limit. This study is further extended to tempered fractional calculus, where tempering ensures finite jump lengths, this is an important remark for unbounded flows. Two tempered definitions are introduced with a smooth and sharp cutoff, by the exponential term and Heaviside function, respectively and we also define the horizon of non-local interactions. We further study the equivalence between the two definitions.
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引用次数: 0
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Journal of Turbulence
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