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Progress in Computational Fluid Dynamics最新文献

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Two dimensional numerical simulations of a free-falling liquid gallium droplet in quiescent water 静止水中自由落体液态镓液滴的二维数值模拟
IF 0.7 4区 工程技术 Q3 Computer Science Pub Date : 2023-01-01 DOI: 10.1504/pcfd.2023.131028
K. Sefiane, M. Mohamad, R. Bennacer
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引用次数: 0
Thermodynamic analysis of Riga plate effect on nanofluid flow in porous medium with nonlinearly varying permeability 渗透率非线性变化的多孔介质中Riga板效应对纳米流体流动的热力学分析
4区 工程技术 Q3 Computer Science Pub Date : 2023-01-01 DOI: 10.1504/pcfd.2023.132220
Lalrinpuia Tlau, Surender Ontela
A comprehensive study of a copper-water nanofluid flowing through a porous medium embedded in an inclined channel is presented in the current article. The permeability of the porous medium is assumed to vary exponentially across the width of the channel. Navier slip at the channel walls is taken into account while the walls are also convectively heated, albeit asymmetrically. The lower wall of the channel is assumed to be made of a Riga plate, a new type of electromagnetic plate made of electrodes and magnets, inducing a plate parallel Lorentz force. Appropriate transformations are applied to the governing equations such that they are non-dimensionalised. The obtained equations are then solved using the homotopy analysis method. For a reduced form of the governing equations, analytical solutions are obtained which are similar to previously presented results. Graphical presentations are discussed for various flow parameters. The impact of the classical Hartman number on the flow is seen to be very significant and can play a pivotal role in reduction of entropy and skin friction. The flow scheme presented in the present article is presented for the first time in literature.
本文对铜-水纳米流体在倾斜通道内多孔介质中的流动进行了全面的研究。假定多孔介质的渗透率沿通道宽度呈指数变化。考虑了通道壁上的纳维尔滑移,同时壁上也受到对流加热,尽管不是对称的。通道的下壁假定是由里加板制成的,里加板是一种由电极和磁铁组成的新型电磁板,可以产生平行的洛伦兹力。适当的变换应用于控制方程,使它们是非量纲化的。然后用同伦分析法对得到的方程进行求解。对于控制方程的简化形式,得到了与先前给出的结果相似的解析解。讨论了各种流动参数的图形表示。经典哈特曼数对流动的影响是非常显著的,可以在减少熵和表面摩擦中起关键作用。本文提出的流动方案在文献中尚属首次。
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引用次数: 1
Numerical investigation of the co-flow jet airfoil on aerodynamic performance 共流射流翼型气动性能的数值研究
4区 工程技术 Q3 Computer Science Pub Date : 2023-01-01 DOI: 10.1504/pcfd.2023.131029
C.M. Vigneswaran, G.C. Vishnu Kumar
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引用次数: 1
Numerical Analysis of Superoleophilic-Superhydrophobic Filtration System for Emulsions Separation Using Lattice Boltzmann Method 晶格玻尔兹曼法分离超亲油-超疏水过滤系统的数值分析
IF 0.7 4区 工程技术 Q3 Computer Science Pub Date : 2023-01-01 DOI: 10.1504/pcfd.2023.10056045
H. Farhat, Luma Al tamimi
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引用次数: 0
Flow separation control in a three-element airfoil system at moderate Reynolds number 中等雷诺数下三元翼型系统流动分离控制
4区 工程技术 Q3 Computer Science Pub Date : 2023-01-01 DOI: 10.1504/pcfd.2023.10058988
Arjun Sharma, Dilip Lalchand Parmar, Deepak Kumar Singh
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引用次数: 0
Pre- and post-stall characteristics of a very light aircraft's wing for different design parameters 非常轻的飞机机翼在不同设计参数下的失速前后特性
4区 工程技术 Q3 Computer Science Pub Date : 2023-01-01 DOI: 10.1504/pcfd.2023.134210
Berkan Anılır, Dilek Funda Kurtuluş
The impact of taper ratio, dihedral angle and wing tip shape on the aerodynamics of a very light aircraft's wing has been investigated by performing URANS simulations at Reynolds number of 5 × 106 for pre- and post-stall conditions. SD 7062 airfoil is selected for the cross-section of the wing geometries investigated. The mean aerodynamic coefficients are found to be invariant to these wing design parameters investigated at low angles of attack. On the other hand, reducing the taper ratio from 1 to 0.5 yields an in-crease in the stall angle of attack and the maximum lift coefficient. The increase of the dihedral angle from 0° to 5° does not lead to any change in the stall angle, however it results a slightly higher maximum lift coefficient with smoother stall behaviour. As evident in the mean surface streamlines, the stall cell formation is observed just above the stall angle for all three wing geometries investigated. The stall cell characteristics with respect to different finite wing design variables and angles of attack are represented and their effects on the sectional lift distributions and total aerodynamic coefficients are discussed.
在5 × 106雷诺数条件下,通过URANS模拟,研究了锥比、二面角和翼尖形状对超轻型飞机机翼失速前后空气动力学特性的影响。SD 7062翼型是选择机翼几何截面的调查。在低迎角情况下,平均气动系数对这些机翼设计参数是不变的。另一方面,将锥比从1减小到0.5会增加失速攻角和最大升力系数。二面角从0°到5°的增加不会导致失速角的任何变化,但是它会导致更高的最大升力系数和更平稳的失速行为。从平均表面流线中可以明显看出,在所有三种机翼几何形状的失速角上方都观察到失速单元的形成。描述了不同有限翼设计变量和迎角下的失速单元特性,并讨论了它们对截面升力分布和总气动系数的影响。
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引用次数: 0
Investigation of upper airway changes in orthognathic surgery with computational fluid dynamics analysis 正颌手术中上呼吸道变化的计算流体动力学分析研究
IF 0.7 4区 工程技术 Q3 Computer Science Pub Date : 2023-01-01 DOI: 10.1504/pcfd.2023.10054095
B. Korbahti, Y. Acar, F. Karkazi, E. Aslan, Ilker Inan, Riza Guven
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引用次数: 0
Unsteady three-dimensional multiphase modeling of anode flow distributor in PEM electrolysis cell PEM电解槽阳极流分布器的非定常三维多相建模
IF 0.7 4区 工程技术 Q3 Computer Science Pub Date : 2023-01-01 DOI: 10.1504/pcfd.2023.10058697
I. Taymaz, S. N. Ozdemir
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引用次数: 0
Variational formulation of incompressible Navier-Stokes equations 不可压缩Navier-Stokes方程的变分公式
4区 工程技术 Q3 Computer Science Pub Date : 2023-01-01 DOI: 10.1504/pcfd.2023.10060376
Akin Ecer
{"title":"Variational formulation of incompressible Navier-Stokes equations","authors":"Akin Ecer","doi":"10.1504/pcfd.2023.10060376","DOIUrl":"https://doi.org/10.1504/pcfd.2023.10060376","url":null,"abstract":"","PeriodicalId":54552,"journal":{"name":"Progress in Computational Fluid Dynamics","volume":null,"pages":null},"PeriodicalIF":0.0,"publicationDate":"2023-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"135613873","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Numerical study of combustion and nitrogen oxide generation for recycled flue gas distribution in supercritical carbon dioxide coal-fired boiler with double furnace 双炉超临界二氧化碳燃煤锅炉循环烟气分布燃烧及氮氧化物生成数值研究
4区 工程技术 Q3 Computer Science Pub Date : 2023-01-01 DOI: 10.1504/pcfd.2023.10060375
Huaqiang Chu, Xiangyong Huang, Mingyan Gu, Yong Wu, Jinyan Yuan, Mingming Wang, Jimin Wang, Lixin Han
{"title":"Numerical study of combustion and nitrogen oxide generation for recycled flue gas distribution in supercritical carbon dioxide coal-fired boiler with double furnace","authors":"Huaqiang Chu, Xiangyong Huang, Mingyan Gu, Yong Wu, Jinyan Yuan, Mingming Wang, Jimin Wang, Lixin Han","doi":"10.1504/pcfd.2023.10060375","DOIUrl":"https://doi.org/10.1504/pcfd.2023.10060375","url":null,"abstract":"","PeriodicalId":54552,"journal":{"name":"Progress in Computational Fluid Dynamics","volume":null,"pages":null},"PeriodicalIF":0.0,"publicationDate":"2023-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"135613874","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
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Progress in Computational Fluid Dynamics
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