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5mm直径翘边孔横向耦合射流轨迹实验

姚尚宏 雷雨冰

姚尚宏, 雷雨冰. 5mm直径翘边孔横向耦合射流轨迹实验[J]. 航空动力学报, 2014, 29(2): 290-297. doi: 10.13224/j.cnki.jasp.2014.02.007
引用本文: 姚尚宏, 雷雨冰. 5mm直径翘边孔横向耦合射流轨迹实验[J]. 航空动力学报, 2014, 29(2): 290-297. doi: 10.13224/j.cnki.jasp.2014.02.007
YAO Shang-hong, LEI Yu-bing. Experiment on coupled jet-in-crossflow trajectory of 5mm diameter warped hole[J]. Journal of Aerospace Power, 2014, 29(2): 290-297. doi: 10.13224/j.cnki.jasp.2014.02.007
Citation: YAO Shang-hong, LEI Yu-bing. Experiment on coupled jet-in-crossflow trajectory of 5mm diameter warped hole[J]. Journal of Aerospace Power, 2014, 29(2): 290-297. doi: 10.13224/j.cnki.jasp.2014.02.007

5mm直径翘边孔横向耦合射流轨迹实验

doi: 10.13224/j.cnki.jasp.2014.02.007
基金项目: 国家自然科学基金(10577011)

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。

     

  • [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.
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出版历程
  • 收稿日期:  2012-12-11
  • 刊出日期:  2014-02-28

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