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矩形扩压通道内流动控制的实验与数值研究 被引量:2

Experimental and Numerical Study on Flow Separation Control in Rectangle Diffuser
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摘要 采用粒子成像测速技术和大涡模拟方法对带有涡旋射流的矩形扩压器分离控制的流场进行了实验和数值分析,数值计算结果与实验数据吻合良好。通过分析实验和计算得到相关截面速度和涡量分布,讨论了涡旋射流的二维涡结构;同时应用三维涡识别技术获得了射流产生各种涡旋结构的流动形态,重点研究射流流向涡结构的生成、发展等动力学演化过程。结果表明:射流剪切层涡系的结构随着时间推移从涡卷演化为了涡环;射流孔口前缘的马蹄涡系具有较强的稳定性,反向涡对具有明显的时均特性。此外还通过对比射流控制前后扩压器表面压力系数、分离区长度、扩张段流动形态及观测点功率谱分析等多种方式探讨了射流控制流动分离的控制效果,并指出射流在下游远场形成的纵向涡旋将主流流场边界层外的高能流体卷入到边界层内,增加了边界层内部的流动能量,从而延缓或抑制了流动分离。 To investigate the mechanism of active control for flow separation in rectangle diffuser by vortex generator jets (VGJs) method,numerical analysis with large-eddy simulation and experimental measurement by particle image velocimetry (PIV) were carried out for the flow field.The numerical results show good agreement with experimental data.The two dimensional vortical structure was discussed in detail via the analysis of their velocity and vorticity distribution.Based on the three dimensional identification of vortex,several vortical structure,with emphasis on the dynamic process of its generation and development,was also discussed.The results show that the jet shear-layer vortices evolved from vortex loops to vortex rings as time go on.Horseshoe vortices wrap around the jet nozzle have the strong stability.The counter-rotating vortex pair has mean-flow definition although they may also have unsteady components.Moreover,to investigate the effect of VGJs on separation control,the surface pressure coefficient,the length of separation zone,the flow characteristics in diffuser and pressure power spectra were compared with and without VGJs.It revealed the longitudinal vortices generate at the downstream of jet increase cross-stream mixing of streamwise momentum and then suppress or delay the separation in diffuser.
出处 《中国电机工程学报》 EI CSCD 北大核心 2010年第5期92-99,共8页 Proceedings of the CSEE
基金 国家自然科学基金项目(10602044) 教育部新世纪优秀人才支持计划项目(NCET-07-0682)~~
关键词 流动控制 涡旋射流 粒子成像测速 大涡模拟 flow control vortex generator jets particle image velocimetry large-eddy simulation
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参考文献19

  • 1Johari H, Rixon G S. Effects of pulsing on a vortex generator jet [J]. AIAAJournal, 2003, 41(12): 2309-2315.
  • 2Johnston J P, Mosier B P, Khan Z U. Vortex generating jets; effects of jet-hole inlet geometry[J]. International Journal of Heat and Fluid Flow, 2002, 23(6):744-749.
  • 3Hasegawa H, Kumagai S. Adaptive separation control system using vortex jets for time-varying flow[J]. Journal of Applied Fluid Mechanics, 2008, 1(2): 9-16.
  • 4Allan B G, Yao C S, Lin J C. Numerical simulations of vortex generator vanes and jets on a flat plate[C]. 1st Flow Control Conference, Missouri, USA, 2002.
  • 5Quinn D, Watterson J K, Crawford A B. Blown jet vortex generator control of a separated diffuser flow[C]. 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, USA, 2006.
  • 6樊涛,谢永慧,张荻.涡旋射流控制扩压器分离流动的大涡模拟[J].中国电机工程学报,2008,28(35):57-65. 被引量:7
  • 7樊未军,易琪,严明,杨茂林.驻涡燃烧室凹腔双涡结构研究[J].中国电机工程学报,2006,26(9):66-70. 被引量:46
  • 8罗坤,陈松,蔡丹云,樊建人,岑可法.气固两相圆柱绕流近场特性的实验研究[J].中国电机工程学报,2006,26(24):116-120. 被引量:12
  • 9Fennema R J, Chaudhry M H. Implicit methods for two-dimensional unsteady free-surface flows[J]. Journal of Hydraulic Research, 1989, 27(3): 321-332.
  • 10姜国强,李炜.横流中有限宽窄缝射流的旋涡结构[J].水利学报,2004,35(5):52-57. 被引量:11

二级参考文献76

共引文献88

同被引文献27

  • 1周冬,任建勋.射流纵向涡强化换热的数值模拟[J].清华大学学报(自然科学版),2004,44(11):1520-1523. 被引量:5
  • 2连祺祥.湍流边界层拟序结构的实验研究[J].力学进展,2006,36(3):373-388. 被引量:27
  • 3叶建,邹正平.逆压梯度下层流分离泡转捩的大涡模拟[J].工程热物理学报,2006,27(3):402-404. 被引量:17
  • 4李雪松,徐建中.低压高负荷涡轮叶栅的大涡模拟[J].工程热物理学报,2007,28(3):403-405. 被引量:4
  • 5BONS J P, SONDERGAARD R, RIVIR R B. Control of low-pressure turbine separation using vortex genera- tor jets, AIAA 99-0367 [R]. Reston, USA: AIAA, 1999.
  • 6BONS J P, SONDERGAARD R, RIVIR R B. Turbine separation control using pulsed vortex generator jets [J]. ASME Journal of Turbomaehinery, 2001, 123 (2) : 198-206.
  • 7RIVIR R B, SONDERGAARD R, BONS J P, et al. Control of separation in turbine boundary layers, AIAA 2004-2201 [R]. Reston, USA: AIAA, 2004.
  • 8GROSS A, FASEL H F. Numerical investigation of low-pressure turbine separation control, AIAA 2008- 4321 [R]. Reston, USA: AIAA, 2008.
  • 9MEMORY C, SNYDERY D O, BONS J. Numerical simulation of vortex generating iets in zero and adverse pressure gradients, AIAA 2008-558[R]. Reston, USA: AIAA, 2008.
  • 10HANSEN L, BONS J. Flow measurements of vortex generator jets in separating boundary layer [J]. Jour- nal of Propulsion and Power, 2006, 22 (3) : 558-566.

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