赵焕娟等：爆轰波三波点擦除烟迹表面积碳机制 341· 糙度和碳迹中积碳颗粒的尺寸 University Press,2008 [17]Zhao H J,Lee J H S,Zhang Y H.Quantitative irregularity anal- 参考文献 ysis for spinning detonation of premixed CHa +202.Chin J Eng,2016,38(11):1552 [Fan B C,Zhang X D,Pan Z H,et al.Fundamental characteris- (赵焕娟，John H.S.LEE,张英华.甲烷预混气螺旋爆轰的 tics of three types of detonation waves utilized in propulsion.Adr 定量不稳定性研究.工程科学学报，2016,38(11)：1552) Meeh,2012,42(2):162 08] Zhang B,Bai C.H.Research progress on the dynamic character- (范宝春，张旭东，潘振华，等.用于推进的三种爆轰波的结 istics of gaseous detonation.Sci Sin Phys Mech Astron,2014,44 构特征.力学进展，2012,42(2)：162) (7):665 Voitsekhovskii B V.Stationary detonation.Dokl USSR Acad Sci, (张博，白春华.气相爆轰动力学特征研究进展.中国科学： 1959,129(6):1254 物理学力学天文学，2014,44(7)：665) B]Bykowski F A,Mitrofanov VV,Vedernikov E F.Continuous det- 09] Zhang B,Mehrjoo N,Ng H D,et al.On the dynamic detonation onation combustion of fuel-air mixtures.Combust Explo Shock parameters in acetyleneoxygen mixtures with varying amount of Wares,1997,33(3):344 argon dilution.Combust Flame,2014,161(5):1390 4]Bykovskii F A,Zhdan S A,Verdemikov E F.Continuous spin 20] Zhang W,Liu Y F,Jiang Z L.Study on the relationship between detonation in ducted annular combustors:2.Combustor with an ignition delay time and gaseous detonation cell size.Chin Theor expanding annular channel.Combust Explo Shock Wares,2008, 4 ppl Mech,2014,46(6):977 44(3):330 (张薇，刘云峰，姜宗林.气相爆轰波胞格尺度与点火延迟 [5]Bykovskii F A,Zhdam S A,Vedemikov E F.Realization and 时间关系研究.力学学报，2014,46(6)：977) modeling of continuous spin detonation of a hydrogen oxygen mix- 21]Wang C J,Xu S L,Fei L S.Study on reaction zone structure of ture in flow-ype combustors.Combust Explo Shock Wares,2009, gaseous detonation wave by planar laser induced fluorescence 45(5):716 technique.Chin J Theor Appl Mech,2007,39(5):661 6]Wang Y H,Wang J P.Coexistence of detonation with deflagration (王昌建，徐胜利，费立森.气相爆轰波反应区结构的平面 in rotating detonation engines.Int J Hydrogen Energy,2016,41 激光诱导荧光测量.力学学报，2007,39(5)：661) (32):14302 [22]Xu X F,Xie L F,Peng J H,et al.Study on the detonation cel- 7]Yang C L,Wu X S,Ma H,et al.Experimental research on initi- lular structure of propylene epoxide-Air.Explos Shock Wares, ation characteristics of a rotating detonation engine.Exp Therm 2004,24(2):158 Fluid Sei,2016,71:154 (徐晓峰，解立峰，彭金华，等.环氧丙烷一空气混合物爆轰 [8]Daniau E,Falempin F,Getin N,et al.Design of a continuous 波胞格结构的研究.爆炸与冲击，2004,24(2)：158) detonation wave engine for space application /42nd AlAA/ [23]Liu S J,Qin H,Lin Z Y,et al.Detailed structure and propaga- ASME/SAE/ASEE Joint Propulsion Conference Exhibit.Califor- ting mechanism research on continuous rotating detonation wave nia,2006:4794 J Propuls Technol,2011,32(3):431 9]Zhang B,Bai C H,Lee J H S.Experimental research on the rela- (刘世杰，覃慧，林志勇，等.连续旋转爆震波细致结构及自 tion of parameters of C2 H-2.502 -Ar mixtures detonation:Criti- 持机理.推进技术，2011,32(3)：431) cal tube diameter,cell size and critical energy of direct initiation [24] Cheng C B,Li J X,Li S M,et al.An experimental study on Trans Beijing Inst Technol,2012,32(3):226 detonation characteristics of binary fuels hydrogen/propaneair (张博，白春华，John H S Lee.C2H2-2.502一Ar混合气体临 mixtures.Explos Shock Wares,2015,35 (2):249 界管径和爆轰胞格及临界能量的实验研究.北京理工大学学 (程关兵，李俊仙，李书明，等.氢气/丙烷/空气预混气体爆 报（自然科学版），2012,32(3)：226) 轰性能的实验研究.爆炸与冲击，2015,35(2)：249) [10]Wu Y W,Lee J H S.Stability of spinning detonation waves 25] Hu X Y,Zhang D L.Variation of the gaseous detonation wave Combust Flame,2015,162(6):2660 through the detonation cell.J Beijing Inst Technol,2001,21 [11]Mazaheri K,Mahmoudi Y,Sabzpooshani M,et al.Experimental (3):2861 and numerical investigation of propagation mechanism of gaseous (胡湘渝，张德良，气相爆轰波贯穿胞格变化研究·北京理 detonations in channels with porous walls.Combust Flame, 工大学学报，2001,21(3)：286) 2015,162(6):2638 [26] Wu Y,Chri Stensen K T.Population trends of spanwise vortices [12]Hishida M,Fujiwara T,Wolanski P.Fundamentals of rotating in wall turbulence.J Fluid Mech,2006,568:55 detonations.Shock Wares,2009,19(1)1 27]Head M R,Bandyopadhyay P.New aspects of turbulent bounda- [13]Zhdan S A,Bykovskii F A,Vedernikov E F.Mathmatical mod- ry-ayer structure.J Fluid Mech,1981,107:297 eling of a rotating detonation wave in a hydrogenoxygen mixture. [28]Yu J L.Gao Y,Yan X O,et al.Correlation between the critical Combust Explos Shock Wares,2007,43(4):449 tube diameter and annular interval for detonation wave in high- [14]Pan Z H,Fan B C,Zhang X D,et al.Wavelet pattern and self- concentration argon diluted mixtures.Explos Shock Waves,2015, sustained mechanism of gaseous detonation rotating in a coaxial 35(4):603 cylinder.Combust Flame,2011,158(11):2220 (喻健良，高远，闫兴清，等.高浓度氢气稀释气体爆轰波临 [15]Trotsyuk A V,Fomin P A,Vasil'ey AA.Numerical study of 界管径和临界间距关系.爆炸与冲击，2015,35(4)：603) cellular detonation structures of methane mixtures.J Loss Prev [29]Zhao H J,Lee J HS,Lee J L,et al.Quantitative comparison of Proc Ind,2015,36:394 cellular pattems of stable and unstable mixtures.Shock Wares, [16]Lee J H S.The Detonation Phenomenon.Cambridge:Cambridge 2016,26(5):621赵焕娟等: 爆轰波三波点擦除烟迹表面积碳机制 糙度和碳迹中积碳颗粒的尺寸． 参 考 文 献 ［1］ Fan B C，Zhang X D，Pan Z H，et al． Fundamental characteris￾tics of three types of detonation waves utilized in propulsion． Adv Mech，2012，42( 2) : 162 ( 范宝春，张旭东，潘振华，等． 用于推进的三种爆轰波的结 构特征． 力学进展，2012，42( 2) : 162) ［2］ Voitsekhovskii B V． Stationary detonation． Dokl USSＲ Acad Sci， 1959，129( 6) : 1254 ［3］ Bykowski F A，Mitrofanov V V，Vedernikov E F． Continuous det￾onation combustion of fuel-air mixtures． Combust Explo Shock Waves，1997，33( 3) : 344 ［4］ Bykovskii F A，Zhdan S A，Verdernikov E F． Continuous spin detonation in ducted annular combustors: 2． Combustor with an expanding annular channel． Combust Explo Shock Waves，2008， 44( 3) : 330 ［5］ Bykovskii F A，Zhdam S A，Vedernikov E F． Ｒealization and modeling of continuous spin detonation of a hydrogen oxygen mix￾ture in flow-type combustors． Combust Explo Shock Waves，2009， 45( 5) : 716 ［6］ Wang Y H，Wang J P． Coexistence of detonation with deflagration in rotating detonation engines． Int J Hydrogen Energy，2016，41 ( 32) : 14302 ［7］ Yang C L，Wu X S，Ma H，et al． Experimental research on initi￾ation characteristics of a rotating detonation engine． Exp Therm Fluid Sci，2016，71: 154 ［8］ Daniau E，Falempin F，Getin N，et al． Design of a continuous detonation wave engine for space application / / 42nd AIAA / ASME / SAE /ASEE Joint Propulsion Conference ＆ Exhibit． Califor￾nia，2006: 4794 ［9］ Zhang B，Bai C H，Lee J H S． Experimental research on the rela￾tion of parameters of C2H2 --2. 5O2 --Ar mixtures detonation: Criti￾cal tube diameter，cell size and critical energy of direct initiation． Trans Beijing Inst Technol，2012，32( 3) : 226 ( 张博，白春华，John H S Lee． C2H2 --2. 5O2 --Ar 混合气体临 界管径和爆轰胞格及临界能量的实验研究． 北京理工大学学 报( 自然科学版) ，2012，32( 3) : 226) ［10］ Wu Y W，Lee J H S． Stability of spinning detonation waves． Combust Flame，2015，162( 6) : 2660 ［11］ Mazaheri K，Mahmoudi Y，Sabzpooshani M，et al． Experimental and numerical investigation of propagation mechanism of gaseous detonations in channels with porous walls． Combust Flame， 2015，162( 6) : 2638 ［12］ Hishida M，Fujiwara T，Wolanski P． Fundamentals of rotating detonations． Shock Waves，2009，19( 1) : 1 ［13］ Zhdan S A，Bykovskii F A，Vedernikov E F． Mathmatical mod￾eling of a rotating detonation wave in a hydrogen-oxygen mixture． Combust Explos Shock Waves，2007，43( 4) : 449 ［14］ Pan Z H，Fan B C，Zhang X D，et al． Wavelet pattern and self￾sustained mechanism of gaseous detonation rotating in a coaxial cylinder． Combust Flame，2011，158( 11) : 2220 ［15］ Trotsyuk A V，Fomin P A，Vasil'ev A A． Numerical study of cellular detonation structures of methane mixtures． J Loss Prev Proc Ind，2015，36: 394 ［16］ Lee J H S． The Detonation Phenomenon． Cambridge: Cambridge University Press，2008 ［17］ Zhao H J，Lee J H S，Zhang Y H． Quantitative irregularity anal￾ysis for spinning detonation of premixed CH4 + 2O2 ． Chin J Eng，2016，38( 11) : 1552 ( 赵焕娟，John H． S． LEE，张英华． 甲烷预混气螺旋爆轰的 定量不稳定性研究． 工程科学学报，2016，38( 11) : 1552) ［18］ Zhang B，Bai C H． Ｒesearch progress on the dynamic character￾istics of gaseous detonation． Sci Sin Phys Mech Astron，2014，44 ( 7) : 665 ( 张博，白春华． 气相爆轰动力学特征研究进展． 中国科学: 物理学力学天文学，2014，44( 7) : 665) ［19］ Zhang B，Mehrjoo N，Ng H D，et al． On the dynamic detonation parameters in acetylene-oxygen mixtures with varying amount of argon dilution． Combust Flame，2014，161( 5) : 1390 ［20］ Zhang W，Liu Y F，Jiang Z L． Study on the relationship between ignition delay time and gaseous detonation cell size． Chin J Theor Appl Mech，2014，46( 6) : 977 ( 张薇，刘云峰，姜宗林． 气相爆轰波胞格尺度与点火延迟 时间关系研究． 力学学报，2014，46( 6) : 977) ［21］ Wang C J，Xu S L，Fei L S． Study on reaction zone structure of gaseous detonation wave by planar laser induced fluorescence technique． Chin J Theor Appl Mech，2007，39( 5) : 661 ( 王昌建，徐胜利，费立森． 气相爆轰波反应区结构的平面 激光诱导荧光测量． 力学学报，2007，39( 5) : 661) ［22］ Xu X F，Xie L F，Peng J H，et al． Study on the detonation cel￾lular structure of propylene epoxide--Air． Explos Shock Waves， 2004，24( 2) : 158 ( 徐晓峰，解立峰，彭金华，等． 环氧丙烷--空气混合物爆轰 波胞格结构的研究． 爆炸与冲击，2004，24( 2) : 158) ［23］ Liu S J，Qin H，Lin Z Y，et al． Detailed structure and propaga￾ting mechanism research on continuous rotating detonation wave． J Propuls Technol，2011，32( 3) : 431 ( 刘世杰，覃慧，林志勇，等． 连续旋转爆震波细致结构及自 持机理． 推进技术，2011，32( 3) : 431) ［24］ Cheng G B，Li J X，Li S M，et al． An experimental study on detonation characteristics of binary fuels hydrogen / propane-air mixtures． Explos Shock Waves，2015，35( 2) : 249 ( 程关兵，李俊仙，李书明，等． 氢气/丙烷/空气预混气体爆 轰性能的实验研究． 爆炸与冲击，2015，35( 2) : 249) ［25］ Hu X Y，Zhang D L． Variation of the gaseous detonation wave through the detonation cell． J Beijing Inst Technol，2001，21 ( 3) : 2861 ( 胡湘渝，张德良． 气相爆轰波贯穿胞格变化研究． 北京理 工大学学报，2001，21( 3) : 286) ［26］ Wu Y，Chri Stensen K T． Population trends of spanwise vortices in wall turbulence． J Fluid Mech，2006，568: 55 ［27］ Head M Ｒ，Bandyopadhyay P． New aspects of turbulent bounda￾ry-layer structure． J Fluid Mech，1981，107: 297 ［28］ Yu J L，Gao Y，Yan X Q，et al． Correlation between the critical tube diameter and annular interval for detonation wave in high￾concentration argon diluted mixtures． Explos Shock Waves，2015， 35( 4) : 603 ( 喻健良，高远，闫兴清，等． 高浓度氩气稀释气体爆轰波临 界管径和临界间距关系． 爆炸与冲击，2015，35( 4) : 603) ［29］ Zhao H J，Lee J H S，Lee J L，et al． Quantitative comparison of cellular patterns of stable and unstable mixtures． Shock Waves， 2016，26( 5) : 621 · 143 ·