[1] |
Kailasanath K.Research on pulse detonation combustion systems:a status report[R].AIAA-2009-631, 2009.
|
[2] |
严传俊, 范玮, 黄希桥.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.
|
[3] |
Petters D P, Felder J L.Engine system performance of pulse detonation concepts using the NPSS program[R].AIAA-2002-3910, 2002.
|
[4] |
Mawid M A, Park T W, Sekar B.Performance analysis of a pulse detonation device as an afterburner[R].AIAA-2000-3474, 2000.
|
[5] |
Mawid M A, Park T W.Towards replacement of turbofan engines afterburners with pulse detonation devices[R].AIAA-2001-3470, 2001.
|
[6] |
Mawid M, Arana C, Park T, et al.Turbofan engine thrust augmentation with pulse detonation afterburners-nozzle influence[R].AIAA-2002-4073, 2002.
|
[7] |
Rasheed A, Furman A H, Dean A J.Experimental investigations of an axial turbine driven by a multi-tube pulsed detonation combustor system[R].AIAA-2005-4209, 2005.
|
[8] |
Andrus I Q, King P I.Evaluation of a high bypass turbofan hybrid utilizing a pulsed detonation combustor[R].AIAA-2007-5074, 2007.
|
[9] |
Pintgen F, Tangirala V.Effect of mixture properties on the performance estimates of a pulse detonation combustor-based hybrid engine[R].AIAA-2007-5391, 2007.
|
[10] |
Fuhua M, Thomas L, Venkat T.Limit cycle investigations of pulse detonation combustor for pulse detonation turbine engine[R].AIAA-2010-6714, 2010.
|
[11] |
Rasheed A, Tangirala V E, Vandervort C L, et al.Interactions of a pulsed detonation engine with a 2D turbine blade cascade[R].AIAA-2004-1207, 2004.
|
[12] |
Nango A, Inaba K, Kojima T.Aerodynamic effect of turbine blade geometry in pulse detonation combustor[R].AIAA-2007-1176, 2007.
|
[13] |
Nango A, Inaba K, Kojima T, et al.Numerical study of detonation interaction with a single-stage axial turbine[R].AIAA-2008-985, 2008.
|
[14] |
Nango A, Inaba K, Kojima T, et al.Numerical study on single-stage axial turbine with pulse detonation combustor[R].AIAA-2009-294, 2009.
|
[15] |
Kojima T, Tsuboi N, Taguchi H, et al.Design study of turbine for pulse detonation combustor[R].AIAA-2007-5081, 2007.
|
[16] |
Xia G, Li D, Merkle C.Modeling of pulse detonation tubes in turbine systems[R].AIAA-2005-0225, 2005.
|
[17] |
Van Zante D, Envia E, Turner M.The attenuation of a detonation wave by an aircraft engine axial turbine stage[R].NASA TM-2007-214972, 2007.
|
[18] |
Hoke J, Bradley R, Stutrud J, et al.Integration of a pulsed detonation engine with an ejector pump and with a turbo-charger as methods to self-asperate[R].AIAA-2002-0615, 2002.
|
[19] |
Schauer F, Bradley R, Hoke J.Interaction of a pulsed detonation engine with a turbine[R].AIAA-2003-0891, 2003.
|
[20] |
Rouser K P, King P I, Schauer F R, et al.Unsteady performance of a turbine driven by a pulse detonation engine[R].AIAA-2010-1116, 2010.
|
[21] |
Rouser K P, Schauer F R, Sondergaard R, et al.Parametric study of unsteady turbine performance driven by a pulse detonation combustor[R].AIAA-2010-6536, 2010.
|
[22] |
Rouser K P, King P I, Schauer F R, et al.Time-accurate flow field and rotor speed measurements of a pulsed detonation driven turbine[R].AIAA-2011-0577, 2011.
|
[23] |
Rouser K P, King P I, Schauer F R, et al.Performance of a turbine driven by a pulsed detonation combustor.Denver, Colorado, US:The ASME 2011 International Mechanical Engineering Congress and Exposition, 2011.
|
[24] |
Rankin B A, Gore J P, Hoke J L, et al.Radiation measurements and temperature estimates of unsteady exhaust plumes exiting from a turbine driven by pulsed detonation combustion[R].AIAA-2013-0886, 2013.
|
[25] |
Rouser K P, King P I, Schauer F R, et al.Experimental performance evaluation of a turbine driven by pulsed detonations[R].AIAA-2013-1212, 2013.
|
[26] |
Rasheed A, Furman A, Dean A J.Experimental investigations of an axial turbine driven by a multi-tube pulsed detonation combustor system[R].AIAA-2005-4209, 2005.
|
[27] |
Baptista M, Rasheed A, Badding B, et al.Mechanical response in a multi-tube pulsed detonation combustor-turbine hybrid system[R].AIAA-2006-1234, 2006.
|
[28] |
Rasheed A, Furman A, Dean A.Wave attenuation and interactions in a pulsed detonation combustor-turbine hybrid system[R].AIAA-2006-1235, 2006.
|
[29] |
Rasheed A, Furman A, Dean A J.Wave interactions in a multi-tube pulsed detonation combustor-turbine hybrid system[R].AIAA-2006-4447, 2006.
|
[30] |
Rasheed A, Furman A H, Dean A J.Pressure measurements and attenuation in a hybrid multi-tube pulse detonation system[J].Journal of Propulsion and Power, 2009, 25(1):148-161.
|
[31] |
Rasheed A, Furman A H, Dean A J.Experimental investigations of the performance of a multitube pulse detonation turbine system[J].Journal of Propulsion and Power, 2011, 27(3):586-596.
|
[32] |
Glaser A J, Caldwell N, Gutmark E.Performance measurements of a pulse detonation combustor array integrated with an axial flow turbine[R].AIAA-2006-1232, 2006.
|
[33] |
Caldwell N, Glaser A, Gutmark E.Acoustic interactions of a pulse detonation engine array with a gas turbine[R].AIAA-2006-1233, 2006.
|
[34] |
Glaser A J, Caldwell N, Gutmark E.Performance of an axial flow turbine driven by multiple pulse detonation combustors[R].AIAA-2007-1244, 2007.
|
[35] |
Caldwell N, Brunet R, Antoine A, et al.Experimental analysis of a hybrid pulse detonation combustor/gas turbine engine[R].AIAA-2008-121, 2008.
|
[36] |
Caldwell N, Gutmark E.Performance analysis of a hybrid pulse detonation combustor/gas turbine system[R].AIAA-2008-4880, 2008.
|
[37] |
Tsukui A, Matsumoto K, Kasahara J, et al.Research on interaction between an intermittent flow and a PDE turbine[R].AIAA-2009-295, 2009.
|
[38] |
Tsuji T, Shirakawa S, Yoshihashi T, et al.Interaction between two cylinders in a pulse detonation engine[J].International Journal of Energetic Materials and Chemical Propulsion, 2009, 8(6):489-500.
|
[39] |
Munday D, George A S, Driscoll R, et al.The design and validation of a pulse detonation engine facility with and without axial turbine integration[R].AIAA-2013-0275, 2013.
|
[40] |
George A S, Driscoll R, Munday D, et al.Experimental investigation of axial turbine performance driven by steady and pulsating flows[R].AIAA-2013-0276, 2013.
|
[41] |
Fernelius M H, Gorrell S E, Hoke J L, et al.Design and fabrication of an experimental test facility to compare the performance of pulsed and steady flow through a turbine[R].AIAA-2013-0277, 2013.
|
[42] |
邓君香, 严传俊, 郑龙席, 等.装有脉冲爆震主燃烧室的燃气涡轮发动机热力性能计算[J].西北工业大学学报, 2008, 26(3):362-367. DENG Junxiang, YAN Chuanjun, ZHENG Longxi, et al.Calculating performance of gas turbine engine with embedded PDC[J].Journal of Northwestern Polytechnical University, 2008, 26(3):362-367.(in Chinese)
|
[43] |
陈文娟, 范玮, 邱华, 等.外涵装有脉冲爆震加力燃烧室的涡扇发动机热力性能分析[J].西北工业大学学报, 2010, 28(2):240-244. CHEN Wenjuan, FAN Wei, QIU Hua, et al.Exploring calculation of thermodynamic performance of the turbo-fan engine with PDCs(pulse detonation combustors) in BD(bypass duct)[J].Journal of Northwestern Polytechnical University, 2010, 28(2):240-244.(in Chinese)
|
[44] |
CHEN Wenjuan, FAN Wei, QIU Hua, et al.Thermodynamic performance analysis of turbofan engine with a pulse detonation duct heater[J].Aerospace Science and Technology, 2011, 23(1):206-212.
|
[45] |
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 detonation wave interacting with turbine blade[J].Journal of Aerospace Power, 2009, 24(1):60-64.(in Chinese)
|
[46] |
郑龙席, 邓君香, 严传俊, 等.混合式脉冲爆震发动机原理性试验系统设计、集成与调试[J].实验流体力学, 2009, 23(1):74-78. ZHENG Longxi, DENG Junxiang, YAN Chuanjun, et al.Design integration and debugging on principle test system of hybrid pulse detonation engine[J].Journal of Experiments in Fluid Mechanics, 2009, 23(1):74-78.(in Chinese)
|
[47] |
DENG Junxiang, ZHENG Longxi, YAN Chuanjun, et al.Experimental investigations of a pulse detonation combustor integrated with a turbine[J].Internationai Journal of Turbo & Jet-Engines, 2008, 25(4):247-257.
|
[48] |
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)
|
[49] |
邓君香, 郑龙席, 严传俊, 等.脉冲爆震燃烧室与涡轮组合的性能试验研究[J].西北工业大学学报, 2009, 27(3):300-304. DENG Junxiang, ZHENG Longxi, YAN Chuanjun, et al.Studying experimentally performances of a pulse detonation combustor(PDC)integrated with a turbine[J].Journal of Northwestern Polytechnical University, 2009, 27(3):300-304.(in Chinese)
|