期刊文献+

弯曲混合管引射系统引射-混合特性数值研究 被引量:7

Numerical Computation for Pumping and Mixing Performance on Mixer-Ejector with Curved Mixing Duct
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摘要 通过三维CFD数值计算,揭示弯曲混合管-波瓣喷管构成的引射混合系统内流场特性,分析了引射系统主要结构参数对引射混合器性能产生的影响。计算结果表明:混合管的弯曲,迫使主流发生偏转,高速主流对壁面冲击,造成近壁面以及混合管内的静压升高,故降低了系统引射流量;高温核心主流随着弯曲引起的二次流向弯管外侧运动,继而向两侧运动,温度等值线最终呈马鞍状。混合管弯曲角度对引射系数影响很大,弯曲角度的增加造成引射流量的迅速减小。弯曲角度大于40°后,混合管出口的热混合效率急剧降低。波瓣瓣宽增加引起混合管截面比减小和主流速度减小,导致引射流量比的急剧减小。随着波瓣扩张角的增大,引射流量比呈先增加后减小趋势。 Based on three-dimen.sional CFD(Computational fluid dynamics) for the lobed mixer-ejector combined with curved mixing duct, internal flow characteristics of the mixer-ejector are discussed, and effects of the main geometry parameters on the lobed mixer-ejector performance are revealed. Results show that the impingement of the primary flow on the curved wall cause the increase of the static pres- sure near the wall and the interior of mixing duct, and the pumping ratio is reduced. The curved angle of the mixing duct is the most significant factor on the pumping ratio. The pumping ratio is rapidly reduced with the increase of the curved angle. And the thermal mixing efficiency is also sharply reduced when the angle exceeds 40^o. As the lobe width is increased, the pumping ratio is sharply decreased by the reduced area ratio of the mixing duct and primary flow velocity. The pumping ratio is enhanced firstly and then decreased with the increase of the lobe penetration angle.
作者 单勇 张靖周
出处 《南京航空航天大学学报》 EI CAS CSCD 北大核心 2008年第2期137-141,共5页 Journal of Nanjing University of Aeronautics & Astronautics
关键词 数值模拟 混合器 引射器 波瓣喷管 弯曲混合管 numerical simulation mixers ejectors lobed nozzle curved mixing duct
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参考文献14

  • 1Presz W M, Reynolds G, McCormick D C. Thrust augment using mixer-ejector-diffuser systems [R]. AIAA Paper 94-0020, 1994.
  • 2Presz W M. Mixer/ejector noise suppressors [R]. AIAA Paper 91-2243, 1991.
  • 3张靖周,李立国,高潮,何文斌.波瓣喷管红外抑制系统的实验研究[J].航空动力学报,1997,12(2):212-214. 被引量:59
  • 4Skebes S A, Paterson R W. Experimental investigation of three-dimensional forced mixer lobe flow fields[R]. AIAA Paper 88-3785-CP, 1988.
  • 5Tsui Y Y,Wu P W. Investigation of the mixing flow structure in multilobe mixers[J]. AIAA Journal, 1996, 34(7): 1386-1391.
  • 6Ooba Y, Kodama H, Nakamura Y. Large eddy simulation analysis of a 18-lobe convoluted mixer nozzle [R]. AIAA Paper 2002-0717, 2002.
  • 7张靖周,谢志荣,李立国.三维强迫混合波瓣结构流场的数值研究[J].推进技术,2001,22(3):225-228. 被引量:12
  • 8Presz W M, Morin B L, Blinn R F. Short efficient ejector systems[R]. AIAA Paper 87-1837, 1987.
  • 9Skebe S A, McCormick D C, Presz W M. Parameter effects on mixer-ejector pumping performance [R]. AIAA Paper 88-0188, 1988.
  • 10张靖周,单勇.二维引射—混合器流场的数值研究与验证[J].航空动力学报,2002,17(5):524-527. 被引量:12

二级参考文献17

  • 1张靖周,李立国,吴国钏.波瓣混合结构三维流场数值计算[J].南京航空航天大学学报,1996,28(6):745-749. 被引量:3
  • 2张靖周,李立国,高潮,何文斌.波瓣喷管红外抑制系统的实验研究[J].航空动力学报,1997,12(2):212-214. 被引量:59
  • 3陶文铨.数值传热学[M].西安:西安交通大学出版社,1992..
  • 4张靖周,航空动力学报,1994年,9卷,1期
  • 5杨致明,南京航空航天大学学报,1994年,26卷,4期
  • 6Skebe S A, McCormick D C, Presz W M. Parameter effects on mi xer-ejector pumping performance[R]. AIAA Paper 88-0188.
  • 7Malecki R E, MItyas S J, Lord W K. Navier-Stokes analysis of an ejector and mixer-ejector operating at pressure ratio in the range 2-4[R]. AIAA P aper 90-2730.
  • 8Liu Y H. Experimental and numerical investigation of circularly lobed no zzle with/without central plug[J].International Journal of Heat and Mass Tra nsfer, 2002,45:2577-2585.
  • 9Presz W M, Reynolds G, McCormick D C. Thrust aug ment using mixer-ejector-diffuser systems [R]. AIAA Paper 94-0020.
  • 10Presz W M. Mixer/ejector noise suppressors[R]. AIAA Pape r 91-2243.

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