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Journal of Applied Fluid Mechanics最新文献

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Sessile Droplet Evaporation on Wall with Radial Temperature Gradient 有径向温度梯度的壁上无水微滴蒸发
IF 1 4区 工程技术 Q3 Engineering Pub Date : 2024-05-01 DOI: 10.47176/jafm.17.05.2193
Z. G. Lei, C. Q. Shen, C. C. Song, F. Yao, X. D. Liu
Droplet evaporation coupled with gravity and surface tension on a wall with the radial temperature gradients is numerically studied with the arbitrary Lagrangian‒Eulerian method. The influence of the wall temperature distribution on the droplet evaporation process, which is less considered in the existing literature, is mainly discussed. The droplet temperature coefficient of the surface tension and the viscosity on the droplet profile evolution, flow, heat and mass transfer characteristic are also discussed. The results indicate that the droplets become flat first and then retract under the gravity and Marangoni convection during droplet evaporation. There are two high-velocity regions inside the evaporating droplet. One region is at the droplet axis, in which fluid flows to the wall from the droplet top. The other region is near the droplet surface, where fluid flows to the droplet top. There are turning points on the two sides of which the influence of wall temperature distribution on the ratio between the droplet height and the radius of the three-phase contact line ( h / R c ), the velocity in the droplet and the surface temperature converts. All of them are larger before the turning point when the wall temperature slope is
采用任意拉格朗日-欧勒方法对具有径向温度梯度的壁面上与重力和表面张力耦合的液滴蒸发进行了数值研究。主要讨论了现有文献较少考虑的壁面温度分布对液滴蒸发过程的影响。此外,还讨论了液滴温度系数、表面张力和粘度对液滴剖面演变、流动、传热和传质特性的影响。结果表明,在液滴蒸发过程中,液滴在重力和马兰戈尼对流作用下先变平后回缩。蒸发液滴内部有两个高速区域。一个区域位于液滴轴线处,液体从液滴顶部流向液滴壁。另一个区域靠近液滴表面,液体流向液滴顶部。两侧存在转折点,转折点上的壁面温度分布对液滴高度与三相接触线半径之比(h/R c)、液滴内速度和表面温度的影响发生了转换。在转折点之前,当壁温斜率为
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引用次数: 0
Study of the Effect of a Cooling Load on a Fluid Surface (Water) in an Open Channel 研究冷却负荷对明渠中流体(水)表面的影响
IF 1 4区 工程技术 Q3 Engineering Pub Date : 2024-05-01 DOI: 10.47176/jafm.17.05.2089
†. A.Leousidis, E. Keramaris, G. Pechlivanidis, Y. Savvidis
In this study the effect of cooling load on the surface water of an open channel with different flow depths is investigated. The method, which was used, involves an experimental laboratory set-up that contains a well-insulated cooling load over a finite area of the water surface, without direct contact with the free water surface so that losses of load to the environment should be avoided. The different cooling loads for each experiment were achieved with the use of insulating films. The insulating film is placed at the bottom of the experimental set-up where there was an empty surface (gap - D), through which the cooling load is allowed to pass. The measurement of velocities was carried out at a two-dimensional (XZ) field, with the help of a digital camera. The recording of motion of the dye (rhodamine) along the channel per unit of time, allows the calculation of the values of the velocity fields. Measurements were conducted when the phenomenon becomes steady. The results for the determination of the cold mass length as a function of the flow depth, and the temperature difference ΔT, in a state of thermal equilibrium, led to the formation of a new mathematical relationship. Further study of the phenomenon is essential for the improvement of this study, in combination with other parameters that affect the aquatic ecosystem.
本研究探讨了冷却负荷对不同水流深度的明渠表层水的影响。所采用的方法是在实验室中设置一个实验装置,在水面的有限区域内包含一个绝缘良好的冷却负载,该负载不与自由水面直接接触,以避免负载损失到环境中。每次实验的不同冷却负荷都是通过使用隔热膜实现的。隔热膜放置在实验装置的底部,那里有一个空的表面(间隙 - D),允许冷却负荷通过。借助数码相机在二维(XZ)场进行速度测量。通过记录染料(罗丹明)在单位时间内沿通道的运动,可以计算出速度场的值。测量是在现象趋于稳定时进行的。在热平衡状态下,冷质量长度的测定结果是流动深度和温差 ΔT 的函数,从而形成了一种新的数学关系。结合影响水生生态系统的其他参数,进一步研究这一现象对改进这项研究至关重要。
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引用次数: 0
Aerodynamic Characterization of Bullet Heads with Different Arcuate Curves 具有不同弧形曲线的弹头的气动特性分析
IF 1 4区 工程技术 Q3 Engineering Pub Date : 2024-05-01 DOI: 10.47176/jafm.17.05.2333
B. Hao, Q. Jiang, C. Xu, L. Liu
The bullet shape is critical in efficient bullet design because it affects the lift and drag forces. This paper proposes a new bullet shape with a logarithmic curve and analyzes the lift and drag coefficients of bullets with different curves under different angles of attack. The results are compared with a bullet whose shape is described by the power law curve. Fluent simulations demonstrate that the optimal power exponent values are 0.65, 0.6, and 0.65 for the bullet with the power law curve and 1.3, 1, and 1 for the bullet with the logarithmic curve at 0°, 30°, and 40° angles of attack, respectively. At a 0° angle of attack, the lift coefficient of the logarithmic curve is the largest. The lift force of the bullet with the logarithmic curve is 129.4% higher than that with the von Karman curve. The drag coefficient is the largest for the bullet with the rectilinear curve; it is 1.30% larger than that of the bullet with the logarithmic curve. At 30° and 40° angles of attack, the lift coefficient of the bullet with the power law curve is larger. The difference in the lift coefficients between the two angles of attack is 18.47%. The bullet’s drag coefficient is the largest for the logarithmic curve, and the difference in the drag coefficients between the two angles of attack is 18.59%.
子弹形状对有效的子弹设计至关重要,因为它会影响升力和阻力。本文提出了一种新的对数曲线子弹形状,并分析了不同攻角下不同曲线子弹的升力和阻力系数。结果与幂律曲线描述形状的子弹进行了比较。流体模拟表明,在 0°、30° 和 40°攻角下,幂律曲线子弹的最佳功率指数值分别为 0.65、0.6 和 0.65,对数曲线子弹的最佳功率指数值分别为 1.3、1 和 1。在 0° 攻角时,对数曲线的升力系数最大。采用对数曲线的子弹升力比采用 von Karman 曲线的子弹升力高 129.4%。直线曲线子弹的阻力系数最大,比对数曲线子弹的阻力系数大 1.30%。在 30° 和 40° 攻角时,幂律曲线子弹的升力系数更大。两个攻角的升力系数相差 18.47%。对数曲线的子弹阻力系数最大,两个攻角的阻力系数相差 18.59%。
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引用次数: 0
Flow Modeling in the Wake of a Francis Turbine with Hydraulic Charge: Case of Songloulou-Cameroon 带水力充注的混流式水轮机尾流的水流模型:松鲁鲁-喀麦隆案例
IF 1 4区 工程技术 Q3 Engineering Pub Date : 2024-04-01 DOI: 10.47176/jafm.17.4.1900
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引用次数: 0
Investigating the Impact of Back Cavity Filling and Axial Clearance on the Flow Physics and Performance of a Pump as Turbine 研究后腔填充和轴向间隙对作为涡轮机的泵的流动物理和性能的影响
IF 1 4区 工程技术 Q3 Engineering Pub Date : 2024-04-01 DOI: 10.47176/jafm.17.4.2256
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引用次数: 1
Effect of Semi-elliptical Outer Blade-surface on the Savonius Hydrokinetic Turbine Performance: A Numerical Investigation 半椭圆形外叶片表面对萨沃尼乌斯水动力涡轮机性能的影响:数值研究
IF 1 4区 工程技术 Q3 Engineering Pub Date : 2024-04-01 DOI: 10.47176/jafm.17.4.2235
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引用次数: 0
Effect of Blade Slot Positioning Close to Blade Root on the Performance of Highly Loaded Helium Compressor 靠近叶片根部的叶片槽位置对高负荷氦气压缩机性能的影响
IF 1 4区 工程技术 Q3 Engineering Pub Date : 2024-04-01 DOI: 10.47176/jafm.17.4.2200
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引用次数: 0
Flow Field Analysis of Francis Turbine Draft Tube using POD at Design and Part Load Operating Conditions 在设计和部分负荷运行条件下使用 POD 对混流式涡轮机通风管进行流场分析
IF 1 4区 工程技术 Q3 Engineering Pub Date : 2024-04-01 DOI: 10.47176/jafm.17.4.2274
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引用次数: 0
Study on the Effect of Bridge Windbreaks on the Aerodynamic Characteristics of High-Speed Trains Meeting under Crosswind 桥梁挡风板对横风条件下高速列车会车空气动力特性的影响研究
IF 1 4区 工程技术 Q3 Engineering Pub Date : 2024-04-01 DOI: 10.47176/jafm.17.4.2204
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引用次数: 0
Investigation of the Flow-Induced Noise and Optimization Design of a Short Tube Throttle Valve 短管节流阀的流量诱发噪声调查与优化设计
IF 1 4区 工程技术 Q3 Engineering Pub Date : 2024-04-01 DOI: 10.47176/jafm.17.4.2018
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引用次数: 0
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Journal of Applied Fluid Mechanics
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