首页 | 本学科首页   官方微博 | 高级检索  
     检索      

低旋流数旋进射流流动特性的PIV实验研究
引用本文:付豪,何创新,刘应征.低旋流数旋进射流流动特性的PIV实验研究[J].实验流体力学,2021,35(3):39-45.
作者姓名:付豪  何创新  刘应征
作者单位:1.上海交通大学机械与动力工程学院 叶轮机械研究所, 上海 200240
基金项目:上海市自然科学基金20ZR1425700
摘    要:采用粒子图像测速技术,研究了当雷诺数Re=4.5×104时低旋流数旋进射流的流动特性。针对3种不同旋流数(S=0、0.26和0.41),对比分析了时均流向速度场、流向速度脉动强度场以及时均涡量场的变化规律。实验测量结果表明:随着旋流数的增加,流向速度大小及其脉动强度沿流向衰减加剧,而射流中心线上的速度脉动强度增强;因腔体壁面空间限制而产生的回流区向上游移动且尺度变小;外剪切层中旋涡的流向发展急剧衰减而内剪切层内的旋涡几乎不受影响。此外,结合速度谱和典型时刻的瞬态流场特征可知,旋流数增大后,旋进频率增大,而旋进现象发生的起始位置向上游移动,使得旋进偏转角度增大。

关 键 词:PIV实验研究    低旋流数    旋进射流    流动特性
收稿时间:2020-10-22

PIV experimental study on flow characteristics of a low swirl number precessing jet
Institution:1.Turbomachinery Research Institute, School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai 200240, China2.Institute of Gas Turbine, Shanghai Jiao Tong University, Shanghai 200240, China
Abstract:This study focuses on the flow characteristics of a low swirl number precessing jet at Reynolds number Re=4.5×104 using particle image velocimetry (PIV). The time-averaged streamwise velocity fields, streamwise velocity fluctuation intensity fields and time-averaged vorticity fields at three swirl numbers, i.e., S=0, 0.26 and 0.41, respectively, are compared and analyzed. The experimental results show that as the swirl number increases, the attenuation of the streamwise velocity and its fluctuation intensity increase along the streamwsie direction, the velocity fluctuation intensity on the jet centerline increases, the recirculation zones caused by the confinement move upstream with their scales decreasing, and the streamwise development of the vortex in the outer shear layer decays rapidly, while that in the inner shear layer is almost unaffected. In addition, combining the streamwise velocity spectrum and the characteristics of the transient flow field at a typical time, it can be seen that as the swirl number increases, the precession frequency increases, and the starting position of the precession phenomenon moves upstream, which increases the precession deflection angle.
Keywords:
点击此处可从《实验流体力学》浏览原始摘要信息
点击此处可从《实验流体力学》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号