期刊文献+

初始压力和狭缝高度对狭缝内起爆距离影响的实验 被引量:1

Experiment on effect of initial pressure and narrow gap height on detonation initiation distance in narrow gap
原文传递
导出
摘要 为获得狭缝内爆轰波起爆距离(DID)的变化规律,分别在宽度为10mm,高度为1.0,2.2,2.9,4.0mm,长度为1220mm的狭缝爆轰管内对不同初始压力下(5~45kPa)化学当量比的乙烯/氧气混气进行单次爆轰性能实验研究.根据烟迹法、高速摄影图片判定起爆位置,得到初始压力和狭缝高度对爆轰波起爆距离的影响规律.结果表明:①在初始压力为10-20kPa时,起爆距离随着狭缝高度增加逐渐缩短;②在初始压力为25~40kPa时,起爆狭缝距离随着狭缝高度变大先降低后增加,在初始压力为45kPa时,起爆距离随着狭缝高度增加而变长;③综合初始压力和狭缝高度的影响,初步得到起爆距离随初始压力和狭缝高度等参数变化的量纲归一化经验公式. Single detonation in stoichiometric ethylene/oxygen mixtures was experimentally studied at initial pressure (5-45 kPa) to achieve change rule of detonation initiation distance (DID) of detonation wave in narrow gap. The narrow gap detonation tube was formed by the cross-section with width of 10mm, height of 1.0, 2.2, 2.9, 4.0mm, and length of 1220 mm. Detonation initiation position was decided by soot records and high-speed digital imaging. Effect law of initial pressure and narrow gap height on detonation initiation distance was achieved. The results indicate that: (1) detonation initiation distance is reduced with the increase of narrow gap height at initial pressure of 10--20kPa; (2) detonation initiation dis- tance initially decreases with increase of narrow gap height and then increases at initial pres- sure of 25--40kPa, and increases at initial pressure of 45kPa with the increase of narrow gap height; (3) compositing the influence of initial pressure and the narrow gap height, non-dimensional empirical formula for detonation initiation distance varying with initial pressure and narrow gap height is achieved.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2015年第9期2066-2072,共7页 Journal of Aerospace Power
基金 国家自然科学基金(51306073 11402102) 江苏省自然基金(BK20130510) 江苏省博士后基金(1301050C)
关键词 微燃烧 微爆轰 狭缝 起爆距离 初始压力 micro-combustion micro-detonation narrow gap initiation distance initial pressure
  • 相关文献

参考文献18

  • 1Kuznetsov M,Alekseev V,Matsukov I,et al.DDT in a smooth tube filled with a hydrogen-oxygen mixture[J].Shock Waves,2005,14(3):205-215.
  • 2Silvestrini M,Genova B,Parisi G,et al.Flame acceleration and DDT run-up distance for smooth and obstacles filled tubes[J].Journal of Loss Prevention in the Process Industries,2008,21(6):555-562.
  • 3Robert B,Detlef A,Rainer G,et al.Effect of ignition position on the run-up distance to DDT for hydrogen-air explosions[J].Journal of Loss Prevention in the Process Industries,2011,24(2):194-199.
  • 4Norton D G,Vlachos D G.Combustion characteristics and flame stability at the microscale:a CFD study of premixed methane/air mixtures[J].Chemical Engineeing Science,2003,58(21):4871-4882.
  • 5Ivanov M F,Kiverin A D,Liberman M A.Hydrogen-oxygen flame acceleration and transition to detonation in channels with no-slip walls for a detailed chemical reaction model[J].Physical Review E,2011,83(5):056313.1-056313.16.
  • 6Akkerman V,Chung K L,Bychkov V,et al.Analysis of flame acceleration induced by wall friction in open tubes[J].Physics of Fluids,2010,22(5):053606.1-053606.14.
  • 7Kagan L,Sivashinsky G.On the transition from deflagration to detonation in narrow tubes[J].Flow Turbulence Combustion,2010,84(3):423-437.
  • 8Wu M H,Wang C Y.Reaction propagation modes in millimeter-scale tubes for ethylene/oxygen mixtures[J].Proceedings of the Combustion Institute,2011,33(2):2287-2293.
  • 9Wu M H,Kuo W C.Accelerative expansion and DDT of stoichiometric ethylene/oxygen flame rings in micro-gaps[J].Proceedings of the Combustion Institute,2013,34(2):2017-2024.
  • 10Nobuyuki T,Youhi M,Hayashi A K.Two-dimensional numerical simulation on galloping detonation in a narrow channel[J].Proceedings of the Combustion Institute,2013,34(2):1999-2007.

二级参考文献32

  • 1何小民,张彭岗,王家骅.爆震管内爆燃到爆震转捩过程的实验研究[J].推进技术,2005,26(3):252-255. 被引量:12
  • 2张永生,周俊虎,杨卫娟,刘茂省,岑可法.微燃烧稳定性分析和微细管道燃烧实验研究[J].浙江大学学报(工学版),2006,40(7):1178-1182. 被引量:14
  • 3王洋,黄蕾,徐斌,吴建,薛宏.低雷诺数下液体的微尺度流动与传热[J].能源技术,2007,28(3):125-128. 被引量:1
  • 4Urtiew P A, Oppenheim A K. Experimental observation of the transition to detonation in an explosive gas[C]// Proceeding Royal Society. London: [s. n.],1966 : 13-38.
  • 5Soloukhin R I. Methods of measurements and main results of experiments in shock tubes [R]. Novosibrisk: Novosibrisk State University Publ. , 1969.
  • 6Smirnov N N, Tyurnikov M V. Experimental investigation of deflagration to detonation transition in hydrocarbon-air gaseous mixtures [J]. Combustion and Flame,1995,100:661-668.
  • 7Thomas G O, Brown C J. Experimental observation of shock-flame interaction leading to DDT[C]//Proc. 7th Conference (International) on Numerical Combustion. New York: [s. n. ], 1998
  • 8Khokhlov A M,Oran E S,Thomas G O. Numerical simulation of deflagration to detonation transition; The role of shock flame interactions in turbulent flames[J]. Combustion and Flame, 1999,117:323-339.
  • 9Sinibaldi J O, Brophy C M, Robinson J P. Ignition effects on deflagration-to-detonation transition in gaseous mixtures[R]. AIAA2000-3590.
  • 10Meyer T R,Hoke J L, Brown M S. Experimental study of deflagration-to-detonation enhancement techniques in a H2/air pulsed detonation engine [R]. AIAA 2002 3270.

共引文献7

同被引文献5

引证文献1

二级引证文献2

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部