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胡建军, 朱晴, 王美达, 金瑶兰, 王思民, 孔祥东. 近距离下射流冲击平板PIV实验研究[J]. 力学学报, 2020, 52(5): 1350-1361. DOI: 10.6052/0459-1879-20-142
引用本文: 胡建军, 朱晴, 王美达, 金瑶兰, 王思民, 孔祥东. 近距离下射流冲击平板PIV实验研究[J]. 力学学报, 2020, 52(5): 1350-1361. DOI: 10.6052/0459-1879-20-142
Hu Jianjun, Zhu Qing, Wang Meid, Jin Yaolan, Wang Simin, Kong Xiangdong. PIV MEASUREMENT OF CLOSE IMPINGING JET ON FLAT PLATE[J]. Chinese Journal of Theoretical and Applied Mechanics, 2020, 52(5): 1350-1361. DOI: 10.6052/0459-1879-20-142
Citation: Hu Jianjun, Zhu Qing, Wang Meid, Jin Yaolan, Wang Simin, Kong Xiangdong. PIV MEASUREMENT OF CLOSE IMPINGING JET ON FLAT PLATE[J]. Chinese Journal of Theoretical and Applied Mechanics, 2020, 52(5): 1350-1361. DOI: 10.6052/0459-1879-20-142

近距离下射流冲击平板PIV实验研究

PIV MEASUREMENT OF CLOSE IMPINGING JET ON FLAT PLATE

  • 摘要: 运用时间分辨粒子成像测速系统(time-resolved particle image velocimetry, TR-PIV)对近距离下射流冲击平板时的流场进行了直接测量, 通过对两个正交的平面流场开展测量, 揭示了冲击距离和雷诺数对射流间隙内三维流动特征及涡系结构演化规律的影响. 结果表明: 射流间隙存在三种典型的涡系结构, 分别为双涡环模式、单涡环模式和卷吸模式, 但在大流量湍流状态下, 射流可能会冲破涡环, 形成随机的高速出流, 各流动模式的出现主要与射流流态及壁面约束作用有关. 运用涡量分析对三种典型涡系结构的能量传递和损失特性进行了比较. 结果表明: 近距离冲击时, 射流的能量通过涡环模式向外传递. 在双涡环模式下, 两个涡环的旋向相反, 端面的约束作用使得两个涡环都被严格约束在射流棒端面之内, 且一次涡环强度显著大于二次涡环强度. 最后, 运用本征正交分解方法对射流间隙内的流动模态及其能量分布进行了分析. 单涡和双涡模式前十阶模态分析结果表明: 能量脉动在较低阶时即以配对的模式出现, 这表明一次涡环与二次涡环均具有良好的对称性, 同时在双涡模式中, 一次涡环是占主导作用的大尺度流动结构. 卷吸模式的前三阶模态分析表明: 射流的能量集中在射流上游, 能量随紊动扩散急剧衰减.

     

    Abstract: The time-resolved particle image velocimetry (TR-PIV) method was used to measure the flow field of a jet impinging on a flat plate in two orthogonal plane at very close distance. The effects of impinging distance and Reynolds number on the flow characteristics and the vortex topology in the clearance were analyzed. The results show that there are three kinds of typical vortex structure in the clearance, namely, double vortex ring mode, single vortex ring mode and complete entrainment mode. However, under the condition of turbulent state with large flow rate, the jet may break through the vortex ring and form random high-speed outflow. The occurrence of each flow pattern is mainly related to the strength of wall constraints. The energy transportation and flow loss of three typical flow patterns are investigated by vorticity analysis. The results show that the energy of the jet is transmitted outward through the vortex-ring mode at close impingement. In the double vortex ring mode, the two vortex rings have opposite rotational direction. Due to the constraint of the end face, both vortex rings are strictly constrained within the end face of the jet nozzle. The strength of the primary vortex ring is significantly greater than that of the secondary vortex ring. Finally, the proper orthogonal decomposition (POD) method is used to analyze the flow mode and energy distribution of the impinging jet. The first ten modal analysis of single and double vortex mode show that the energy fluctuation occurs in a paired pattern at a lower order, which indicates that both the primary and secondary vortex rings have good symmetry. Meanwhile, in the double vortex ring mode, the primary vortex ring is the dominant large-scale flow structure. The first three modes of the complete entrainment mode show that the energy of the jet is concentrated in the upstream of the jet and decreases sharply with the turbulent diffusion.

     

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