Experiment on coupled jet-in-crossflow trajectory of 5mm diameter warped hole
-
摘要: 采用粒子图像测速仪(PIV)对5mm直径翘边孔横向耦合射流流场进行了研究,实验结果表明:射流入射角与翘边孔角度有较大的偏差,但是随着翘边孔角度的增加,射流入射角增大;引入翘边孔射流有效直径,由试验数据得到了有效直径的数值。对射流轨迹曲线进行了拟合,考虑了两种主通道气流速度、四种不同角度的翘边孔和三种不同深度的主通道,方程式能较好地反映小尺寸通道翘边孔射流的流动结构,为今后的流场设计提供依据。Abstract: Particle image velocimetry (PIV) was used for learning the 5mm diameter warped hole flow field in jet-in-crossflow. The result shows that: the jet angle differs from the warped hole angles, the larger of the warped hole angle means the larger jet angle; there will be a useful parameter named effective diameter from the experiment data. Jet flow trajectory curves were fitted in condition of two types of velocity, four different warped hole angles and three tunnels with different depth. The curve is well fitted with the real jet flow, contributing to the future flow field design in micro combustors or other small tunnels.
-
[1] McGuirk J J, Spencer A.Coupled and uncoupled CFD prediction of the characteristics of jets from combustor air admissio ports[J].Journal of Engineering for Gas Turbines and Power, 2001, 123(2):327-332. [2] Haven B A, Kurosaka M.Kidney and anti-kidney vortices in crossflow jets[J].Journal of Fluid Mechanics, 1998, 352:27-64. [3] Johari H, Pacheco-Tougas M Y, Hermanson J C.Penetration and mixing of fully modulated turbulent jets in crossflow[J].AIAA Journal 1999, 37(7):842-850. [4] Han D, Orozco V.Gross-entrainment behavior of turbulent jets injected obliquely into a uniform cross flow[J].AIAA Journal, 2000, 38(9):1643-1649. [5] 王卫东.横喷射流与空气混合增强的实验研究[J].推进技术, 1998, 19(3):52-56. WANG Weidong.Experimental study on mixing enhancement of vortex generator jets[J].Journal of Propulsion Technology, 1998, 19(3):52-56.(in Chinese) [6] Ligrani P M, Wigle J M, Jackson S W.Film-cooling from holes with compound angle orientations:Part 2 results downstream a single row of holes with 6d span wise spacing[J].ASME Journal of Heat Transfer, 1994, 116(2):353-362. [7] Spencer A, McGuirk J J.LDA measurements of feed annulus effects on combustor liner port flows[J].Journal of Fluids Engineering, 2001, 123(2):219-227. [8] 张勃, 吉洪湖, 黄伟, 等.圆转矩形喷管射流掺混特性实验[J].航空动力学报, 2009, 24(11):2476-2482. ZHANG Bo, JI Honghu, HUANG Wei, et al.Experimental investigation of mixing characteristics of jet from circle-rectangular transition nozzle[J].Journal of Aerospace Power, 2009, 24(11):2476-2482.(in Chinese) [9] 郭婷婷, 刘建红, 宋东辉, 等.不同形状气膜孔对气膜冷却效果的影响[J].动力工程, 2006, 26(3):333-336. GUO Tingting, LIU Jianhong, SONG Donghui, et al.Influence of jet orifice geometry on film cooling effectiveness[J].Journal of Power Engineering, 2006, 26(3):333-336.(in Chinese) [10] 李少华, 宋东辉, 刘建红, 等.不同孔型平板气膜冷却的数值模拟[J].中国电机工程学报, 2006, 26(17):112-116. LI Shaohua, SONG Donghui, LIU Jianhong, et al.Numerical simulations of flat plate film cooling using respectively different shaped jet holes[J].Proceedings of the CSEE, 2006, 26(17):112-116.(in Chinese) [11] 郭婷婷, 徐忠, 李少华.2种角度横向紊动射流的实验分析[J].西安交通大学报, 2003, 37(11):1208-1210. GUO Tingting, XU Zhong, LI Shaohua.Experimental study on turbulent jets injected obliquely into a crossflow[J].Journal of Xi'an Jiaotong University, 2003, 37(11):1208-1210.(in Chinese) [12] 郭婷婷, 金建国, 李少华, 等.不同出射角度对气膜冷却流场的影响[J].中国电机工程学报, 2006, 26(16):117-121. GUO Tingting, JIN Jianguo, LI Shaohua, et al.A numerical simulation in film cooling flows with different injection angles[J].Proceedings of the CSEE, 2006, 26(16):117-121.(in Chinese) [13] 李念, 张堃元, 沙江.应用PIV技术测量压电型自耦合射流[J].航空学报, 2007, 28(1):20-24. LI Nian, ZHANG Kunyuan, SHA Jiang.Experiments on the characteristics and structure of unsteady flow field of synthetic jet[J].Acta Aeronautica et Astronautica Sinica, 2007, 28(1):20-24.(in Chinese) [14] 李念, 张堃元, 徐惊雷, 等.自耦合射流对平行主射流的矢量偏转PIV实验[J].航空动力学报, 2006, 21(4):675-680. LI Nian, ZHANG Kunyuan, XU Jinglei, et al.Experimental investigation of primary flow vectoring using parallel self-coupling jets[J].Journal of Aerospace Power, 2006, 21(4):675-680.(in Chinese) [15] Subramanya K, Porey P D.Trajectory of a turbulent cross flow[J].Hydraulic Research, 1984, 22(5):343-354.
点击查看大图
计量
- 文章访问数: 1560
- HTML浏览量: 9
- PDF量: 1025
- 被引次数: 0