[1] |
Mastorakos E.Ignition of turbulent non-premixed flame[J].Progress in Energy and Combustion Science,2009,35(1):57-97.
|
[2] |
李大鹏,潘余,吴继平.几何可调喉道双模态冲压发动机点火过程试验研究[J].弹箭与制导学报,2006,26(4):210-217. LI Dapeng,PAN Yu,WU Jiping.Ignition experimental study of a variable geometrical throat dual-mode ramjet[J].Journal of Projectiles,Rockets,Missiles and Fuidance,2006,26(4):210-217.(in Chinese)
|
[3] |
Neophytou A,Richardson E S,Mastroakos E.Spark ignition of turbulent recirculating non-premixed gas and spray flames:a model for predicting ignition probability[J].Combustion and Flame,2012,159(4):1503-1522.
|
[4] |
Aggarwal S K.A review of spray ignition phenomena:present status and future research[J].Progress in Energy and Combustor Science,1998,24(6):565-600.
|
[5] |
Whitehurst R B,Krauss R H,McDaniel J C.Parametric and time resolved studies of autoignition and flame holding in a clean air supersonic combustor[R].AIAA-92-3424,1992.
|
[6] |
李庆.基于凹腔火焰稳定器的亚燃冲压发动机燃烧室点火过程研究[D].长沙:国防科学技术大学,2010 LI Qing.Research on the ignition process of cavity-based flameholder in ramjet combustor[D].Changsha:National University of Defense Technology,2010.(in Chinese)
|
[7] |
Yang V,Li J,Choi J Y,et al.Ignition transient in an ethylene fueled scramjet engine with air throttling[R].AIAA 2010-410,2010.
|
[8] |
Yu K,Wilson K J,Smith R A,et al.Experimental investigation on dual-purpose cavity in supersonic reacting flows[R].AIAA 1998-723,1998.
|
[9] |
Owens M G,Tehranian S,Segal C,et al.Flame-holding configurations for kerosene combustion in a Mach 1.8 airflow[J].Journal of Propulsion and Power,1998,14(4):456-461.
|
[10] |
Kobayashi K,Tomiokat S,Mitani T.Supersonic flow ignition by plasma torch and H2/O2 torch[J].Journal of Propulsion and Power,2004,20(2):294-301.
|
[11] |
宋文艳,刘伟雄,贺伟.超声速燃烧室等离子体点火实验研究[J].实验流体力学,2006,20(4):20-24 SONG Wenyan,LIU Weixiong,HE Wei.Experimental investigation of plasma ignition in supersonic combustor[J].Journal of Experiments in Fluid Mechanics,2006,20(4):20-24.(in Chinese)
|
[12] |
Lewis B,Elbe G.Combustion,flames and explosions of gases.[M].London:Harcourt Brace Jovanovich Publishers,1987.
|
[13] |
席文雄.超声速气流中的点火启动及其强化机理研究[D].长沙:国防科学技术大学,2013. XI Wenxiong.Investigation on initiation of ignition and mechanism for enhancement in supersonic flowfield[D].Changsha:National University of Defense Technology,2013.(in Chinese)
|
[14] |
Gruber M R,Donbar J M,Carter C D,et al.Mixing and combustion studies using cavity-based flameholders in a supersonic reacting flows[J].Journal of Propulsion and Power,2004,20(5):769-779.
|
[15] |
Rasmussen C C,Driscoll J F,Carter C D,et al.Characteristics of cavity stabilized flames in a supersonic flow[J].Journal of Propulsion and Power,2005,21(4):765-769.
|
[16] |
Rasmussen C C,Driscoll J F,Hsu K Y.Stability limits of cavity-stabilized flames in supersonic flow[J].Proceedings of the Combustion Institute,2005,30(2):2825-2834.
|
[17] |
Mohamed M C,Kurian J.Cavity-based injections into supersonic flow[J].Journal of Propulsion and Power,2005,21(6):1130-1132.
|
[18] |
Mathur T,Gruber M R,Jackson K.Supersonic combustion experiments with a cavity-based fuel injector[J].Journal of Propulsion and Power,2001,17(6):1305-1312.
|
[19] |
O'Byrne S,Stotz I,Neely A J,et al.OH PLIF imaging of supersonic combustion using cavity injection[R].AIAA 2005-3357,2005
|
[20] |
Sick V.High speed imaging in fundamental and applied combustion research[J].Proceedings of the Combustion Institute,2013,34(2):3509-3530.
|
[21] |
Schmit R F,Semmelmayer L F,Haverkamp L M,et al.Fourier analysis of high speed shadowgraph images around a Mach 1.5 cavity flow field[R].AIAA 2011-3961,2011.
|
[22] |
Sun M B,Gong C,Zhang S P,et al.Spark ignition process in a scramjet combustor fueled by hydrogen and equipped with multi-cavities at Mach 4 flight condition[J].Experimental Thermal and Fluid Science,2012,43(11):90-96.
|