期刊文献+

超声速流中凹腔交错布置流场研究

Interaction Between Interleaved Installation Cavities in Supersonic Flow
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摘要 利用高速摄影仪和纹影仪,对超声速流中两凹腔火焰稳定器交错布置的流场结构进行了实验研究。结果表明,凹腔间相互作用主要体现为激波的相互作用,两凹腔间波系相互作用,使各自流场结构发生变化;两相同短凹腔或长凹腔交错布置,凹腔各自波系增强;短凹腔和长凹腔交错布置,各自波系都减弱。 Interaction between two interleaved installation cavities in supersonic flow was experimentally investigated with high speed camera and schlieren system. Results revealed that shock interaction was main affec^on between two cavities, shock interaction between two cavities lead to the change of cavities flowfield;double cavities with same length range(short or long) will strengthen the compression shock or expansion shock; different length cavities combine will decrease the flow strength.
出处 《国防科技大学学报》 EI CAS CSCD 北大核心 2009年第4期98-101,共4页 Journal of National University of Defense Technology
基金 国家高技术基金资助项目
关键词 超声速燃烧冲压发动机 凹腔 纹影 激波相互干扰 scramjet cavity schlieren shock interaction
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参考文献6

  • 1Cain T, Walton C. Review of Experiments on Igntition and Flaraeholding in Supersonic Flow[R]. AIAA 2002 - 3877,2002.
  • 2Ben-Yakar A, Hanson R K. Cavity Flame-holders for Ignition and Flame Stabilization in Scrarnjets: An Overview[J]. JPP, 2001,14(4):869- 877.
  • 3刘欧子,胡欲立,蔡元虎,刘敬华,凌文辉.超声速燃烧凹槽火焰稳定的研究动态[J].推进技术,2003,24(3):265-271. 被引量:21
  • 4Gmber M R, Baurle R A, Mathur T, et al. Fundamental Studies of Cavity-based Flameholder Concepts for Supersonic Combustors[ R]. AIAA 99 - 2248,1999.
  • 5Vinagradov V, Kobigsky S A, Petrov M D. Experimental Investigation of Kerosene Fule Combustion in Supersonic How[J]. J. of propulsion and power, 1991, 11(1):130-134.
  • 6Nedungadi A, Lewis M J. A Numerical Study of Fuel Mixing Enhancement Using an Oblique Shock/Vortex Interaction[ R]. AIAA 96 - 2920,1996.

二级参考文献38

  • 1胡欲立.超声速燃烧的实验研究与数值模拟[M].西安:西北工业大学,1995..
  • 2Mathur T, Streby G, Gruber M, et al. Supersonic combustion experiments with a cavity-based fuel injector[R]. AIAA 99-2102.
  • 3Yu G, Li G J, Chang X Y, et al. Investigation of kerosene combustion characteristic with pilot hydrogen in model supersonic combustors [ J ]. Journal of Propulsion and Power,2001,17(6) : 1263 - 1272.
  • 4Lin J C, Rockwell D. Organized oscillations of initially turbulent flow past a cavity[J]. AIAA Journal, 2001,39(6) : 1139 -1151.
  • 5Ben Yakar A, Hanson R K. Experimental investigation of flame-holding capability of a transverse hydrogen jet in supersonic cross-flow [ C]. Proceeding of the Twenty-Seventh International Symposium on Combustion, Combustion Inst. Pittsburgh, PA, 1998:2173 - 2180.
  • 6Riggins D W, McClinton C R, Bittner R C. Investigation of scramjet injection strategies for high Mach number flows[J].Journal of Propulsion and Power, 1995,11 (3) .409 - 418.
  • 7McMillin B K, Seitzman J M, Hanson R K. Comparison of NO and OH planar fluorescence temperature measurements in scramjet model flow fields [ J]. AIAA Journal, 1994, 32(10) : 1945- 1952.
  • 8John D A, Corin S, James C, et al. Experimental supersonic hydrogen combustion employing staged behind a rearwardfacing step[J]. Journal of Propulsion and Power, 1993,9(3) :472 -478.
  • 9Donohue J M, McDaniel J C, Haj-Hariri H. Experimental and numerical study of swept ramp injection into a supersonic flowfield[J]. AIAA Journal, 1994,32(9): 1860 - 1867.
  • 10Gerligradov P, Brilggemann. Numerical investigation of hydrogen strut injections into supersonic airflows [ J]. Journal of Propulsion and Power, 2000,16(1): 22-28.

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