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The experimental investigation on dynamic response of free surface for non-isothermal liquid bridge with the varying shear airflow

机译:不同剪切气流非等温液体桥的自由面动态响应的实验研究

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Through high-speed camera and the self-developed software package for interface recognition, the space-time evolution of free surface has been investigated for non-isothermal liquid bridge with shear airflow, and the dynamic response of free surface to the shear airflow has also been analyzed. When the shear airflow is induced from the upper disk (u 0), the convex part of free surface is oppressed downward to the gas side by the shear airflow, which increases the curvature of concave part on the free surface. Under the condition of u 0, the convex part of free surface is pulled upward to the gas side by the shear airflow, which also exacerbates the curvature of concave part on the free surface. The experimental results show that the shear airflow is introduced from upper disk increasing the probability of dam break for the liquid bridge. The deformation of free surface is intensified with the accelerated shear airflow. Due to the different initial free surface shapes (different volume ratios), the direction and intensity of shear stress vary at the different positions of free surface, and the dynamic response law of the free surface deformation is also different. For a liquid bridge with the volume ratio less than 1 (V = 0.802, V = 0.899), the deformation of free surface presents a certain sinusoidal rule. When the volume ratio of liquid bridge is larger than 1 (V = 1.071), under shear airflow induced from upper disk, the deformation of free surface is still presents sinusoidal rule. When the velocity of shear airflow is u 0 (u = 1 m/s, u = 1.5 m/s, u = 2.0 m/s), the convex part of free surface moves up by the lifting action of shear airflow, and the shape of free surface presents multi-peak structure. For the liquid bridge with the large aspect ratio (Gamma = 1.4), the convex region occupies most part of the interface, and there is no change for the free surface shape under the effect of shear airflow. The free surface shape still presents upper conc
机译:通过高速摄像机和用于接口识别的自主开发的软件包,已经研究了具有剪切气流的非等温液体桥的空间时间演化,并且自由表面与剪切气流的动态响应也有分析了。当从上盘引起剪切气流时(U <0),通过剪切气流向下压制自由表面的凸部,该剪切气流将凹部的凹部增加到自由表面上。在U&gt的条件下;如图0所示,自由表面的凸部通过剪切气流向上拉到气体侧,这也使凹入部分的曲率加剧在自由表面上。实验结果表明,剪切气流从上盘引入液体桥的坝断裂概率。通过加速剪切气流加强自由表面的变形。由于初始自由表面形状(不同体积比),剪切应力的方向和强度在自由表面的不同位置变化,并且自由表面变形的动态响应规律也不同。对于体积比小于1(v = 0.802,v = 0.899)的液体桥,自由表面的变形呈现出某个正弦规则。当液体桥的体积比大于1(v = 1.071)时,在从上盘引起的剪切气流下,自由表面的变形仍然存在正弦规则。当剪切气流的速度是u&gt时; 0(u = 1 m / s,u = 1.5 m / s,u = 2.0 m / s),自由表面的凸部通过剪切气流的提升作用来移动,自由表面的形状呈现多峰结构体。对于具有大纵横比(伽马= 1.4)的液体桥,凸起区域占据界面的大部分,并且在剪切气流的效果下没有变化的自由表面形状。自由表面形状仍然存在上浓度

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