| Citation: | Numerical study on matching mechanism and efficiency ofpulse detonation combustor and impulse turbine[J]. Journal of Aerospace Power, 2018, 33(8): 1864-1871. doi: 10.13224/j.cnki.jasp.2018.08.009
|
| [1] |
严传俊,范玮.脉冲爆震发动机原理及关键技术［M］.西安：西北工业大学出版社,2005.
|
| [2] |
郑龙席,卢杰,严传俊,等.脉冲爆震涡轮发动机研究进展［J］.航空动力学报,2014,29(5):993-1000.ZHENG Longxi,LU Jie,YAN Chuanjun,et al.Research progress on pulse detonation turbine engine［J］.Journal of Aerospace Power,2014,29(5):993-1000.(in Chinese)
|
| [3] |
李晓丰,郑龙席,邱华,等.两相脉冲爆震涡轮发动机原理性试验［J］.航空动力学报,2013,28(12):2731-2736.LI Xiaofeng,ZHENG Longxi,QIU Hua,et al.Two phase pulse detonation turbine engine original rational test［J］.Journal of Aerospace Power,2013,28(12):2731-2736.(in Chinese)
|
| [4] |
邓君香,郑龙席,严传俊,等.脉冲爆震燃烧室与涡轮相互作用的试验［J］.航空动力学报,2009,24(2):307-312.DENG Junxiang,ZHENG Longxi,YAN Chuanjun,et al.Experimental investigations of interaction of a pulse detonation combustor with a turbine［J］.Journal of Aerospace Power,2009,24(2):307-312.(in Chinese)
|
| [5] |
ZANTE D V,ENVIA E,TURNER M G.The attenuation of a detonation wave by an aircraft engine axial turbine stage［R］.NASA/TM-2007-214972,2007.
|
| [6] |
NANGO A,INABA K,KOJIMA T,et al.Aerodynamic effect of turbine blade geometry in pulse detonation combustor［R］.AIAA-2007-1176,2007.
|
| [7] |
FERNELIUS M,GORRELL S,HOKE J,et al.Design and fabrication of an experimental test facility to compare the performance of pulsed and steady flow through a turbine［R］.AIAA-2013-0886,2013.
|
| [8] |
黄玥.脉冲爆震发动机喷管性能的数值模拟研究［D］.南京:南京航空航天大学,2008.HUANG Yue.Numerical simulation of nozzle performance in pulse detonation engine［D］.Nanjing:Nanjing University of Aeronautics and Astronautics,2005.(in Chinese)
|
| [9] |
严传俊,何立明,范玮,等.脉冲爆震发动机的研究与发展［J］.航空动力学报,2001,16(3):212-217.YAN Chuanjun,HE Liming,FAN Wei,et al.Research and development of pulse detonation engine［J］.Journal of Aerospace Power,2001,16(3):212-217.(in Chinese)
|
| [10] |
李晓丰,郑龙席,邱华.脉冲爆震燃烧室与径向涡轮相互作用数值模拟研究［C］∥第三届爆轰与爆震发动机研讨会.西安:中国航空学会,2013:76-80.
|
| [11] |
楚武利,刘前智,胡春波,航空叶片机原理［M］.西安：西北工业大学出版社,2009：150.
|
| [12] |
邹正平.航空燃气轮机涡轮气体动力学［M］.上海：上海交通大学出版社,2014.
|
| [13] |
华琛,嘉诺塔.内燃机涡轮增压器原理［M］.北京：中国铁道出版社,1990.
|
| [14] |
张睿刚.超高膨胀比涡轮机气动性能研究［D］.哈尔滨:哈尔滨工业大学,2014.ZHANG Ruigang.Research on aerodynamic performance of ultra-high expansion turbine［D］.Harbin:Harbin Institute of Technology,2014.(in Chinese)
|
| [15] |
罗俊,何立明,陈灯.二维爆震波数值模拟［J］.推进技术,2008,29(1):29-32.LUO Jun,HE Liming,CHENG Deng.Numerical simulation of two-dimensional detonation wave［J］.Journal of Propulsion Technology,2008,29(1):29-32.
|
| [16] |
蒋彬,罗凯,高爱军,等.一种微型部分进气冲动式涡轮机设计方法［J］.鱼雷技术,2015,23（5）:353-358.JIANG Bin,LUO Kai,GAO Aijun,et al.Design method of a miniature partial intake impulse turbine［J］.Torpedo Technology,2015,23（5）:353-358.(in Chinese)
|
| [17] |
赵寅生.鱼雷涡轮机原理［M］.西安: 西北工业大学出版社,2002.
|
| [18] |
刘广涛.大膨胀比涡轮级内流场数值研究［D］.哈尔滨:哈尔滨工业大学,2012.LIU Guangtao.Numerical simulation of turbulent flow in large expansion ratio［D］.Harbin:Harbin Institute of Technology,2014.
|
| [19] |
舒士甄.叶轮机械原理［M］.北京:清华大学出版社,1991.
|
| [20] |
蒋联友,严传俊,邓君香,等.爆震波与涡轮叶片相互作用的数值模拟［J］.航空动力学报,2009,24(1):60-64.JIANG Lianyou,YAN Chuanjun,DENG Junxiang,et al.Numerical simulation of the interaction between detonation wave and turbine blade［J］.Journal of Aerospace Power,2009,24(1):60-64.(in Chinese)
|
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