Effect of Kerosene Distribution on Combustion Performance in Supersonic Combustor
Air-breathing Hypersonic Technology Research Center,China Aerodynamics Research and Development Center, Mianyang 621000,China;Air-breathing Hypersonic Technology Research Center,China Aerodynamics Research and Development Center, Mianyang 621000,China;Air-breathing Hypersonic Technology Research Center,China Aerodynamics Research and Development Center, Mianyang 621000,China
[2] 甘晓华.航空燃气轮机燃油喷嘴技术[M].北京:国防工业出版社,2008. [3] Ben Yakar A, Hanson R K.Cavity Flameholders for Ignition and Flame Stabilization in Scramjet:Review and Experimental Study[R].AIAA 1998-3122. [4] Mather G Streby.Supersonic Combustion Experiments with a Cavity-Based Fuel Injector [R].AIAA 1999-2102. [5] Johe M Seiner, Dash S M.Historical Survey on Enhanced Mixing in Scramjet Engine [R].AIAA 1999-4869. [6] Takeshi Kanda.Study of the Intensive Combustion in the Scramjet Engine [R].AIAA 1998-3123. [7] Li Jian, Ma Fuhua, Yang Vigor.A Comprehensive Study of Ignition Transient in an Ethylene-Fueled Scramjet Combustor[R].AIAA 2007-5025. [8] 宋文艳,刘伟雄,贺伟,等.超声速燃烧室等离子体点火实验研究[J].实验液体力学,2006,20(4). [9] 俞刚,李建国,陈立红,等.煤油-氢双燃料超声速燃烧点火特性研究[J].液体力学实验与测量,0,4(1):63-71. [10] 覃川,傅维标.少量H2对预混气着火的影响[J].燃烧科学与技术,0,6(2):179-184. [11] 林宇震,许全宏,刘高恩.燃气轮机燃烧室[M].北京:国防工业出版社,2008. [12] 严传俊,范玮.燃烧学[M].西安:西北工业大学出版社,2005. [13] 余勇,丁猛,刘卫东.煤油超声速燃烧的实验研究[J].国防科技大学学报,2004,26(1). [14] 陈思员,徐旭.当量比对单凹腔超燃燃烧室流场影响的三维数值模拟[J].航空学报,2009,30(5).