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激励射流在超声速流场中的混合特性研究 被引量:1

EXPERIMENTAL INVESTIGATION OF THE EXCITED JET IN SUPERSONIC MIXING
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摘要 将Hartmann-Sprenger(H-S)管集成到传统射流装置中形成激励射流,研究其在超声速流场中的混合特性.设计了3种频率的CO_2激励射流,将其横向注入Ma=2.5的均匀超声速来流当中.采用平面激光散射技术对其进行瞬态可视化成像,利用组分采样进行时均分析.结果表明:H-S激励射流可以有效提高射流穿透深度,形成较多大尺度结构,从而获得较好的混合效果. Hartmann-Sprenger(H-S) tube could generate oscillated flow with high frequency and high amplitude under JRG mode.This article made an excited jet by putting H-S tube into the traditional jet device to investigate its effects on the supersonic mixing.The CO_2 jets excited under three different frequencies were injected into the Mach 2.5 supersonic flow.Planar laser scattering was used to visualize the instantaneous flow while sampling the concentration of CO_2 was used to obtain the time-averaged results.The results showed that the excited jet improved the depth of jet penetration,and made much more large-scale structures,so that it got better mixing in the supersonic flow,especially in the 1 kHz-excited case.
出处 《力学学报》 EI CSCD 北大核心 2010年第5期957-961,共5页 Chinese Journal of Theoretical and Applied Mechanics
基金 国家自然科学基金资助项目(90305022 10525212 10621202)~~
关键词 激励射流 超声速混合 穿透深度 大尺度结构 excited jet supersonic mixing depth of penetration the large-scale structure
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参考文献5

  • 1Randolph H, Chew L, Johari H. Pulsed jets in cross flow. J Propul Power, 1994, 10:746-748.
  • 2Murugappan S, Gutmark E. Control of penetration and mixing of an excited supersonic jet into a supersonic cross stream. Physics of Fluids, 2005, 17(10): 106101-106113.
  • 3顾声龙,陈立红,张新宇.H-S管激励振荡流动的数值模拟及实验研究[J].实验流体力学,2009,23(4):1-6. 被引量:3
  • 4Lee MP, McMillin BK, Palmer JL, et al. Two-dimensional imaging of combustion phenomena in a shock tube using planar laser-induced fluorescence. AIAA Paper, 91-0460, 1991.
  • 5Lee MP, McMillin BK, Palmer JL, et al. Planar fluorescence imaging of a transverse jet in a supersonic cross flow. Journal of Propulsion and Power, 1992, 8(4): 729-735.

二级参考文献6

  • 1VIRENDRA S LILYD H. Experimental investigation of flow and heating in a resonance tube[J].J. Fluid Mech. 1979, (94):669- 672.
  • 2BROCHER E, MARESCA C, BOURNAY M H. Fluid dynamics of the resonance tube [ J ]. J. Fluid Mech. 1970, (43) : 369-384.
  • 3MURUGAPPAN S, GUTMARK E. Parametric study of the Hartmann-Sprenger tube [J].Experiments in Fluids, 2005,38,813- 283.
  • 4CAIN A B, KERSCHEN E J, RAMAN Get al. Simulation of powered resonance tubes [ C ] // 1st Flow Control Conference 24-26 June 2002, St. Louis, Missouri.
  • 5MORCH K A. A theory for the mode of operation of the Hartmann air jet generator[J]. J. Fluid Mech. 1964, (20) : 141-159.
  • 6BLUCH D J, CULTER A D. Investigation of a Hartmann-Sprenger tube for passive heating of scramjet injectant gases [ C]//41st Aerospace Sciences Meeting and Exhibit6-9 January 2003, Reno, Nevada .

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