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Journal of Turbulence最新文献

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A comparative study of bandpass-filter-based multi-scale methods for turbulence energy cascade 基于带通滤波器的湍流能量级联多尺度方法比较研究
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-09-11 DOI: 10.1080/14685248.2024.2400953
Aditya Anand, Sourabh S. Diwan, Nedunchezhian Swaminathan
Two different bandpass filtering methods have been used in the literature to study turbulence energy cascade simultaneously in physical and scale spaces. One of them is the derivative-based filter ...
文献中使用了两种不同的带通滤波方法来同时研究物理空间和尺度空间中的湍流能量级联。其中一种是基于导数的滤波 ...
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引用次数: 0
On the physical structure, modelling and computation-based prediction of two-dimensional, smooth-wall turbulent boundary layers subjected to streamwise pressure gradients 受流向压力梯度影响的二维平滑壁湍流边界层的物理结构、建模和基于计算的预测
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-08-19 DOI: 10.1080/14685248.2024.2392572
Klewicki Joseph, Sandberg Richard, Knopp Tobias, Devenport William, Fritsch Daniel, Vishwanathan Vidya, Volino Ralph, Toxopeus Serge, McKeon Beverley, Eca Luis
This paper reports on the recent NATO Advanced Vehicle Technology (AVT) effort associated with smooth-wall two-dimensional turbulent boundary layer flows subjected to streamwise pressure gradients....
本文报告了最近北约先进飞行器技术(AVT)与受流向压力梯度影响的光滑壁二维湍流边界层流相关的工作....。
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引用次数: 0
Large-eddy simulation of shock train in convergent-divergent nozzles with isothermal walls 带等温壁的汇聚-发散喷嘴中冲击列的大涡流模拟
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-08-13 DOI: 10.1080/14685248.2024.2388314
Agneev Roy, Somnath Ghosh
High-order accurate Large-eddy simulations (LES) have been carried out for compressible, turbulent flow through two bell-shaped convergent-divergent nozzles- one with a short divergent portion and ...
针对流经两个钟形收敛-发散喷嘴的可压缩湍流,我们进行了高阶精确大涡流模拟(LES),其中一个喷嘴的发散部分较短,另一个喷嘴的发散部分较长。
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引用次数: 0
Uniform momentum zones in turbulent channel flow 湍流通道流中的均匀动量区
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-08-03 DOI: 10.1080/14685248.2024.2387847
Jianda Huang, Yucheng Jie, Chunxiao Xu, Lihao Zhao
The characteristics of uniform momentum zones (UMZs) and UMZ interfaces in turbulent channel flow (TCF) at friction Reynolds number ranging from 600 to 2000 are investigated. The focus is on the Re...
研究了摩擦雷诺数在 600 到 2000 之间的湍流通道流(TCF)中均匀动量区(UMZs)和均匀动量区界面的特征。研究的重点是雷诺数的变化。
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引用次数: 0
Transient energy transfer and cascade analysis for stratified turbulent channel flows 分层湍流通道流的瞬态能量传递和级联分析
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-07-09 DOI: 10.1080/14685248.2024.2377162
Kiran Jadhav, Abhilash J. Chandy
A comprehensive and fine-grained transient analysis of the kinetic budget equation in the spectral and spatial domains for channel flow subjected to stable stratification is performed, through a se...
本研究对稳定分层条件下渠道流的动力学预算方程的频谱域和空间域进行了全面、精细的瞬态分析,并通过se...
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引用次数: 0
Rough bed hydrodynamics under wave-current interactional flow field: double averaging approach 波流相互作用流场下的粗糙床流体力学:双重平均法
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-07-01 DOI: 10.1080/14685248.2024.2371824
Jayanta Shounda, Krishnendu Barman, Koustuv Debnath
The effect of surface wave on the double-averaged (DA) current-only flow properties is examined over two different types of rough beds comprising hemispherical elements with regular and staggered a...
研究了表面波对两种不同类型粗糙床面的双平均(DA)纯流特性的影响,这两种粗糙床面分别由规则和交错的半球形元件组成。
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引用次数: 0
Reynolds number effect on the Lagrangian evolution of hairpin vortices in turbulent channel flow 雷诺数对湍流通道流中发夹涡的拉格朗日演化的影响
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-06-25 DOI: 10.1080/14685248.2024.2363886
Behnam Kazemi Majd, Zeinab Pouransari
The evolution and generation of hairpins are studied in a Lagrangian perspective in turbulent channel flows. Direct numerical simulation database of turbulent channel flow at friction Reynolds numb...
从拉格朗日的角度研究了湍流通道流中毛刺的演变和生成。在摩擦雷诺数条件下湍流通道流的直接数值模拟数据库可用于研究湍流通道流中毛刺的演变和产生。
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引用次数: 0
Evaluation of subgrid-scale models in decaying rotating stratified turbulence 衰变旋转分层湍流中的亚网格尺度模型评估
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-06-18 DOI: 10.1080/14685248.2024.2367507
Kiran Jadhav, Rahul Agrawal, Abhilash J. Chandy
The results of large eddy simulation (LES) using four sub-grid scale (SGS) models, namely: constant coefficient Smagorinsky (CS), dynamic Smagorinsky (DS), a dynamic Clark (DC) model, and dynamic L...
使用四种子网格尺度(SGS)模型,即恒定系数斯马戈林斯基(CS)、动态斯马戈林斯基(DS)、动态克拉克(DC)模型和动态L...
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引用次数: 0
Challenges and perspective on the modelling of high-Re, incompressible, non-equilibrium, rough-wall boundary layers 高褶皱、不可压缩、非平衡、粗糙壁边界层建模的挑战与展望
IF 1.9 4区 工程技术 Q1 Engineering Pub Date : 2024-06-04 DOI: 10.1080/14685248.2024.2361738
R. García-Mayoral, Daniel Chung, Paul Durbin, Nicholas Hutchins, T. Knopp, B. McKeon, U. Piomelli, Richard D. Sandberg
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引用次数: 0
Errors and uncertainties in CFD validation for non-equilibrium turbulent boundary layer flows at high Reynolds numbers 高雷诺数下非平衡湍流边界层流动的 CFD 验证误差与不确定性
IF 1.9 4区 工程技术 Q3 MECHANICS Pub Date : 2024-05-30 DOI: 10.1080/14685248.2024.2360195
T. Knopp, L. Eça, S. L. Toxopeus, D. Fritsch, A. Gargiulo, K. T. Lowe, C. J. Roy, G. Deng, M. Visonneau, E. Guilmineau
NATO AVT-RTG-349 was dedicated to the validation of computational fluid dynamics (CFD) methods based on the Reynolds-Averaged Navier-Stokes (RANS) equations and statistical turbulence models for no...
北约AVT-RTG-349致力于验证基于雷诺平均纳维-斯托克斯(RANS)方程和统计湍流模型的计算流体动力学(CFD)方法,该方法适用于无...
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引用次数: 0
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Journal of Turbulence
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