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JOURNAL OF FLOW VISUALIZATION AND IMAGE PROCESSING最新文献

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Damped flow-induced vibrations of a square cylinder at low Reynolds numbers 低雷诺数下方形圆柱体的阻尼流激振动
IF 0.6 Q4 ENGINEERING, MECHANICAL Pub Date : 2022-01-01 DOI: 10.1615/jflowvisimageproc.2022041335
P. Yadav, Sachin Sharma, Subhankar Sen
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引用次数: 1
Transient characteristics of the trailing jet of a compressible vortex ring at Mach 1.5 马赫数为1.5马赫时可压缩涡环尾部射流的瞬态特性
IF 0.6 Q4 ENGINEERING, MECHANICAL Pub Date : 2022-01-01 DOI: 10.1615/jflowvisimageproc.2022041772
Javed Mohd., T. Murugan, D. Das
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引用次数: 1
A review on unsteady fluid-flexible structure interaction 非定常流体-柔性结构相互作用研究进展
IF 0.6 Q4 ENGINEERING, MECHANICAL Pub Date : 2022-01-01 DOI: 10.1615/jflowvisimageproc.2022040041
K. Sharma, S. Dutta
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引用次数: 1
Plume Analysis of Plunging Liquid Jets with Floor Interactions using Stereographic Backlit Imaging 利用立体背光成像分析具有底板相互作用的俯冲液体射流的羽流
IF 0.6 Q4 ENGINEERING, MECHANICAL Pub Date : 2022-01-01 DOI: 10.1615/jflowvisimageproc.2022044942
Roy A. Pillers, T. Heindel
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引用次数: 0
Convolutional Neural Networks for Problems in Transport Phenomena: a Theoretical Minimum 传输现象问题的卷积神经网络:理论最小值
IF 0.6 Q4 ENGINEERING, MECHANICAL Pub Date : 2022-01-01 DOI: 10.1615/jflowvisimageproc.2022043908
Arjun Bhasin, A. Mistry
{"title":"Convolutional Neural Networks for Problems in Transport Phenomena: a Theoretical Minimum","authors":"Arjun Bhasin, A. Mistry","doi":"10.1615/jflowvisimageproc.2022043908","DOIUrl":"https://doi.org/10.1615/jflowvisimageproc.2022043908","url":null,"abstract":"","PeriodicalId":41984,"journal":{"name":"JOURNAL OF FLOW VISUALIZATION AND IMAGE PROCESSING","volume":"1 1","pages":""},"PeriodicalIF":0.6,"publicationDate":"2022-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"67576804","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Investigate the exhaust gas flow of a match rocket with schlieren photography 用纹影照相法研究火柴火箭的废气流动
IF 0.6 Q4 ENGINEERING, MECHANICAL Pub Date : 2022-01-01 DOI: 10.1615/jflowvisimageproc.2022042653
A. Lozano, Yun Liu
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引用次数: 0
Numerical Flow Visualization: Vista and Expedition 数值流可视化:Vista和远征
IF 0.6 Q4 ENGINEERING, MECHANICAL Pub Date : 2022-01-01 DOI: 10.1615/jflowvisimageproc.2022040403
Zhanping Liu
Numerical flow visualization resorts to data processing, feature extraction, geometric construction, image synthesis, graphical display, and scene manipulation to enable intuitive insightful interactive analysis of tangential directions of movement embedded in a velocity vector field. This paper presents some advances in numerical flow visualization over the past three decades, with emphasis on geometry-based and texture-based methods. Also introduced in this context is our own research for representing, depicting, and exploring flow data. Not intended for an exhaustive survey of the literature, our discussions revolve around streamline integration, interactive streamline placement, automatic streamline placement (including evenly spaced layout of streamlines), streamline clustering, time-dependent flow lines (e.g., pathlines), flow texture synthesis (e.g., line integral convolution), feature mining (e.g., flow topology), and parallel visualization. These topics address flows ranging from planar to surface and volumetric domains, from steady to unsteady cases, and from Cartesian to curvilinear and unstructured grids. This scope allows us to examine a variety of approaches in the working mechanism, numerical accuracy, representation effectiveness, visual quality, and computational performance so as to show the respective advantages and disadvantages. The findings may help visualization researchers pinpoint main long-lasting challenges, visualization developers identify practically applicable techniques, and domain scientists perceive important promising advances in numerical flow visualization.
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引用次数: 0
AN EXPERIMENTAL STUDY ON SHOCK CELL STRUCTURES OF UNDEREXPANDED JETS FROM CORRUGATED LOBED NOZZLES USING THE SCHLIEREN IMAGING TECHNIQUE 采用纹影成像技术对波纹叶喷嘴欠膨胀射流激波室结构进行了实验研究
IF 0.6 Q4 ENGINEERING, MECHANICAL Pub Date : 2022-01-01 DOI: 10.1615/jflowvisimageproc.v29.i4.30
K. G. Kriparaj, V. P. Roy, P. Tide, N. Biju
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引用次数: 1
Reduced-order modelling of non-canonical laminar wakes 非规范层流尾迹的降阶模型
IF 0.6 Q4 ENGINEERING, MECHANICAL Pub Date : 2022-01-01 DOI: 10.1615/jflowvisimageproc.2022040226
I. Paul, K. A. Prakash, S. Vengadesan
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引用次数: 0
FLOW PAST STATIONARY AND OSCILLATING AIRFOIL AT A LOW REYNOLDS NUMBER USING SHARP INTERFACE IMMERSED-BOUNDARY APPROACH 用锐界面浸没边界方法研究低雷诺数下静止和振荡翼型的流动
IF 0.6 Q4 ENGINEERING, MECHANICAL Pub Date : 2021-02-10 DOI: 10.1615/JFlowVisImageProc.2020030995
P. Seshadri, A. De
The present study reports on flow past airfoils (stationary and moving) using sharp interface immersed-boundary approach. Non-boundary conforming approach like immersed-boundary method offers a viable alternative over traditional boundary conforming approach by allowing us to model flow past arbitrarily complex shapes, by eliminating the need to re-grid the flow domain as the body exhibits motion. We present flow past a NACA 0012 airfoil at stationary conditions as well as exhibiting pitching motion. Evolution of vortex dynamics and wake structures are presented to show that the developed sharp interface immersed-boundary approach captures the flow physics of dynamic stall accurately. Moving body problems involving immersed-boundary approach usually encounter the issues of spurious oscillations and mass conservation. This is handled through a field extension strategy based on ghost cell approach, which allows for extrapolating the flow field value onto the ghost nodes, ensuring smooth temporal transition as the immersed surface moves through time. The results presented here show excellent agreement with the experimental results found in the literature.
本研究报告的流动通过翼型(静止和运动)使用尖锐界面浸入边界方法。非边界一致性方法,如浸入边界方法,提供了一种可行的替代传统的边界一致性方法,允许我们模拟任意复杂形状的流动,通过消除需要重新网格化的流动领域,因为身体表现出运动。我们现在流过一个NACA 0012翼型在静止条件下,以及展示俯仰运动。涡动力学和尾迹结构的演变表明,所提出的尖锐界面浸入边界方法能够准确地捕捉动态失速的流动物理特性。涉及浸入边界方法的动体问题通常会遇到伪振荡和质量守恒问题。这是通过基于鬼影单元方法的场扩展策略来处理的,该策略允许将流场值外推到鬼影节点上,确保浸入表面随时间移动时的平滑时间过渡。本文给出的结果与文献中的实验结果非常吻合。
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引用次数: 3
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JOURNAL OF FLOW VISUALIZATION AND IMAGE PROCESSING
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