| Citation: | ZENG Hao, HE Li-ming, RONG Kang, ZHANG Qiang. Experiment on shock wave focus in resonator[J]. Journal of Aerospace Power, 2012, 27(12): 2655-2659.
|
| [1] |
Eidelman B S.Pulse detonation engine:a status review and technology development road map[R].AIAA-97-2740,1997.
|
| [2] |
Levin V A,Nechaev J N,Tarasov A I.A new approach to organizing operation cycles in pulse detonation engines[C]//High Speed Deflagration and Detonation:Fundamentals and Control.Moscow:ELEX-KM Publishers,2001:223-238.
|
| [3] |
Tarasov A I,Pushkin R M,Levin V A,et al.Method and device for obtaining thrust:Russia,PU2034996C[P].1995-09-23.
|
| [4] |
Cooper M,Shepherd J E.Experiments studying thermal cracking,catalytic cracking,and pre-mixed partial oxidation of JP-10[R].AIAA-2003-4867,2003.
|
| [5] |
Leyva I V,Tangirala V.Investigation of unsteady flow field in a 2-stage PDE resonator[R].AIAA-2003-715,2003.
|
| [6] |
Keith R M,Dean M A J.Experimental evaluation of a two-stage pulse detonation combustor[R].AIAA-2005-3773,2005.
|
| [7] |
王栋.脉冲爆震发动机工作过程数值模拟研究[D].南京:南京理工大学,2007.WANG Dong.Numerical simulation of working process of pulse detonation engine[D].Nanjing:Nanjing University of Science and Technology,2007.(in Chinese)
|
| [8] |
姜日红,武晓松,王栋.共振型PDE 谐振腔喷嘴匹配关系研究 [J].航空动力学报,2009,24(5):1006-1010.JIANG Rihong,WU Xiaosong,WANG Dong.Matching research of resonat PDE's resonator and jet[J].Journal of Aerospace Power,2009,24(5):1006-1010.(in Chinese)
|
| [9] |
周鸿.两步法高频爆震发动机(two-stage PDE)机理与特性研究[D].南京:南京航空航天大学,2008.ZHOU Hong.Performance study of two-stage PDE[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2008.(in Chinese)
|
| [10] |
李海鹏.两级脉冲爆震发动机中激波会聚起爆过程的数值模拟研究[D].西安:空军工程大学,2010.LI Haipeng.Simulation study of shock wave focusing of two stage pulse detonation engine[D].Xi'an Air Force Engineering University,2010.(in Chinese)
|
| [11] |
曾昊,何立明,章雄伟,等.环形射流喷口位置对激波聚焦起爆的影响分析[J].空气动力学学报,2011,32(3):437-442.ZENG Hao,HE Liming,ZHANG Xiongwei,et al.Investigation on the influence of jets spout location on detonation initiation via imploding annular shock waves[J].Journal of Prpulsion Technology,2011,32(3):437-442.(in Chinese)
|
| [12] |
李海鹏,何立明,陈鑫,等.不同结构形式凹面腔内的激波会聚起爆爆震波数值研究[J].兵工学报,2009,30(增刊):203-206.LI Haipeng,HE Liming,CHEN Xin,et al.Numerical simulation of detonation initiation at the convergence of shock waves induced by annular centripetal jets in different concave reflectors[J].Acta Armamentarii,2009,30(sup.):203-206.(in Chinese)
|
| [13] |
曾昊,何立明,章雄伟,等.环形射流初始压力对激波聚焦起爆爆震的影响分析[J].航空动力学报,2010,25(9):1964-1970.ZENG Hao,HE Liming,ZHANG Xiongwei.Investigation on the influence of jets pressure on detonation initiation via imploding annular shock waves[J].Journal of Aerospace Power,2010,25(9):1964-1970.(in Chinese)
|
| [14] |
曾昊,何立明,章雄伟,等.入射喷口宽度对环形射流激波聚焦起爆爆震的影响分析[J].空气动力学学报,2011,29(4):501-507.ZENG Hao,HE Liming,ZHANG Xiongwei,et al.Investigation on the influence of jet width on detonation initiation via imploding annular shock waves[J].Acta Aerodynamica Sinica,2011,29(4):501-507.(in Chinese)
|
| [15] |
曾昊.两级脉冲爆震发动机的实验研究与数值模拟[D].西安:空军工程大学,2011.ZENG Hao.Experimental study and numerical simulation of two-stage pulse detonation engine.[D].Xi'an:Air Force Engineering University,2011.(in Chinese)
|
DownLoad: