[1] |
姜宗林,滕宏辉,刘云峰.气相爆轰物理的若干研究进展[J].力学进展,2012,42(2):129-140. JIANG Zonglin,TENG Honghui,LIU Yunfeng.Some research process on gaseous detonation physics[J].Advances in Mechanics,2012,42(2):129-140.(in Chinese)
|
[2] |
Lee J H,Knystautas R,Yoshikawa N.Photochemical initiation of gaseous detonation[J].Acta Astronautica,1978,5(11/12):971-982.
|
[3] |
Knystautas R,Lee J H,Moen I,et al.Direct initiation of spherical detonation by a hot turbulent gas jet[C]//Seventeenth Symposium (International) on Combustion.England:Symposium (International) on Combustion,1979:1235-1245.
|
[4] |
Moen I O,Bjerketvedt D,Engebretsen T,et al.Transition to detonation in a flame jet[J].Combustion and Flame,1989,75(3/4):297-308.
|
[5] |
Carnasciali F,Lee J H S,Knystautas R,et al.Turbulent jet initiation of detonation[J].Combustion and Flame,1991,84(1/2):170-180.
|
[6] |
Dorofeev S B,Bezmelnitsin A V,Sidorov V P,et al.Turbulent jet initiation of detonation in hydrogen-air mixtures[J].Shock Waves,1996,6(1):73-78.
|
[7] |
Krok J C.Jet initiation of deflagration and detonation[D].California:California Institute of Technology,1997.
|
[8] |
Lieberman D H,Parkin K L,Shepherd J E.Detonation initiation by a hot turbulent jet for use in pulse detonation engines[R].AIAA-2002-3909,2002.
|
[9] |
Brophy C M,Werner L T S,Sinibaldi J O.Performance characterization of a valveless pulse detonation engine[R].AIAA-2003-1344,2003.
|
[10] |
于军力,秦亚欣,高歌.射流点火对爆震管中爆燃转爆震影响的实验[J].航空动力学报,2011,26(5):1043-1047. YU Junli,QIN Yaxin,GAO Ge.Experimental investigation on effects of flame jet ignition on deflagration to detonation transition in tube[J].Journal of Aerospace Power,2011,26(5):1043-1047.(in Chinese)
|
[11] |
李建玲,范玮,李强,等.火焰射流点火起爆的实验探索[J].燃烧科学与技术,2009,15(5):461-465. LI Jianling,FAN Wei,LI Qiang,et al.Experimental investigation on detonation initiation by flame jet[J].Journal of Combustion Science and Technology,2009,15(5):461-465.(in Chinese)
|
[12] |
曾昊,何立明,章雄伟,等.横向爆震射流起爆爆震过程的数值模拟[J].应用力学学报,2010,27(3):543-549. ZENG Hao,HE Liming,ZHANG Xiongwei,et al.Simulation of transverse detonation jet initiation process[J].Chinese Journal of Applied Mechanics,2010,27(3):543-549.(in Chinese)
|
[13] |
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)
|
[14] |
曾昊,何立明,章雄伟,等.环形射流初始压力对激波聚焦起爆的影响分析[J].航空动力学报,2010,25(9):1964-1970. ZENG Hao,HE Liming,ZHANG Xiongwei,et al.Investigation on the influence of jet pressure on detonation initiation via imploding annular shock waves[J].Journal of Aerospace Power,2010,25(9):1964-1970.(in Chinese)
|
[15] |
Ishii K,Kataoka H,Kojima T.Initiation and propagation of detonation waves in combustible high speed flows[J].Proceedings of the Combustion Institute,2009,32(2):2323-2330.
|
[16] |
韩旭,周进,林志勇,等.超声速预混气的热射流起爆过程数值模拟[J].推进技术,2012,33(4):650-656. HAN Xu,ZHOU Jin,LIN Zhiyong,et al.Numerical investigation of detonation initiation by a hot jet in supersonic premix flow[J].Journal of Propulsion Technology,2012,33(4):650-656.(in Chinese)
|
[17] |
HAN Xu,ZHOU Jin,LIN Zhiyong.Experimental investigations of detonation initiation by hot jets in supersonic premixed flows[J].Chinese Physics:B,21(12):124702.1-124702.5.
|
[18] |
HAN Xu,ZHOU Jin,LIN Zhiyong,et al.Deflagration-to-detonation transition induced by hot jets in a supersonic premixed airstream[J].Chinese Physics Letters,2013,30(5):054701.1-054701.3.
|
[19] |
Berger M.Adaptive mesh refinement for hyperbolic differential equations[D].Stanford:Stanford University,1982.
|
[20] |
Berger M,Oliger J.Adaptive mesh refinement for hyperbolic partial differential equations[J].Journal of Computational Physics,1984,53(3):484-512.
|
[21] |
Deiterding R.Parallel adaptive simulation of multi-dimensional detonation structures[D].Cottbus:Brandenburgischen Technischen University,2003.
|
[22] |
Deiterding R.High-resolution numerical simulation and analysis of Mach reflection structures in detonation waves in low-pressure H2-O2-Ar mixtures:a summary of results obtained with the adaptive mesh refinement framework AMROC[EB/OL].[2013-07-10].Http://dx.doi.org/10.1155/2011/738969.
|
[23] |
CAI Xiaodong,LIANG Jianhan,LIN Zhiyong,et al.Adaptive mesh refinement based numerical simulation of detonation initiation in supersonic combustible mixtures using a hot jet[EB/OL].[2013-09-01].Http://dx.doi.org/10.1061/(ASCE)AS.1943-5525.0000376.
|
[24] |
CAI Xiaodong,LIANG Jianhan,LIN Zhiyong,et al.Influence analysis of geometrical parameters of detonation initiation with a hot jet by adaptive mesh refinement method[R].AIAA-2013-4167,2013.
|
[25] |
Liang Z,Browne S,Deiterding R,et al.Detonation front structure and the competition for radicals[J].Proceedings of the Combustion Institute,2007,31(2):2445-2453.
|
[26] |
Westbrook C K.Chemical kinetics of hydrocarbon oxidation in gaseous detonations[J].Combustion and Flame,1982,46:191-210.
|
[27] |
Strehlow R A.Gas phase detonations:recent developments[J].Combustion and Flame,1968,12(2):81-101.
|
[28] |
Goodwin D.Cantera:object-oriented software for reacting flows[EB/OL].[2013-07-10].Http://www.cantera.org.
|
[29] |
Hu X Y,Khoo B C,Zhang D L,et al.The cellular structure of a two-dimensional H2/O2/Ar detonation wave[J].Combustion Theory and Modelling,2004,8(2):339-359.
|