[1]王放,翁春生,李宝星,等.连续旋转爆轰波传播过程试验研究[J].固体火箭技术,2018,41(06):688-693.
 ANG Fang,WENG Chunsheng,LI Baoxing,et al.Experimental investigation on the propagation process of continuous rotating detonation wave[J].Journal of Solid Rocket Technology,2018,41(06):688-693.
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连续旋转爆轰波传播过程试验研究

参考文献/References:

[1]Lu F K,Braun E M. Rotating detonation wave propulsion: experimental challenges,modeling,and engine concepts[J].Journal of Propulsion & Power,2011,30(5): 1-18.

[2]Bykovskii F A,Zhdan S A,Vedernikov E F.Reactive thrust generated by continuous detonation in the air ejection mode[J].Combustion,Explosion,and Shock Waves,2013,49(2): 188-195.
[3]Bykovskii F A,Zhdan S A.Current status of research of continuous detonation in fuel-air mixtures (Review)[J].Combustion,Explosion,and Shock Waves,2015,51(1): 21-35.
[4]Frolov S M,Aksenov V S,Dubrovskii A V,et al.Energy efficiency of a continuous-detonation combustion chamber[J].Combustion,Explosion,and Shock Waves,2015,51(2): 232-245.
[5]Frolov S M,Aksenov V S,Ivanov V S,et al.Large-scale hydrogen-air continuous detonation combustor[J].International Journal of Hydrogen Energy,2015,40(3): 1616-1623.
[6]Dyer R,Naples A,Kaemming T,et al.Parametric testing of a unique rotating detonation engine design[R].AIAA 2012-0121.
[7]Thomas L M,Schauer F R,Hoke J L.Naples,buildup and operation of a rotation detonation engine[R].AIAA 2011-0602.
[8]刘世杰,林志勇,林伟,等.H2/Air连续旋转爆轰波的起爆及传播过程试验[J].推进技术,2012,33(3): 483-489.LIU Shijie,LIN Zhiyong,LIN Wei,et al.Experiment on the ignition and propagation processes of H2/Air continuous rotating detonation wave[J].Journal of Propulsion Technology,2012,33(3): 483-489.
[9]刘世杰.连续旋转爆震波结构、传播模态及自持机理研究[D].长沙:国防科技大学,2013.LIU Shijie.Investigations on the structure,rotating mode and lasting mechanism of continuous rotating detonation wave[D]. Changsha:National University of Defense Technology,2013.
[10]Zhang H L,Liu W D,Liu S J.Experimental investigations on H2/air rotating detonation wave in the hollow chamber with Laval nozzle[J].International Journal of Hydrogen Energy,2017,42(5): 3363-3370.
[11]郑权,翁春生,白桥栋.倾斜环缝喷孔式连续旋转爆轰发动机试验[J].推进技术,2014,35(4): 570-576.[JP2]ZHENG Quan,WENG Chunsheng,BAI Qiaodong.Experiment on continuous rotating detonation engine with tilt slot injector[J].Journal of Propulsion Technology,2014,35(4) : 570-576.[12]郑权,翁春生,白桥栋.当量比对液体燃料旋转爆轰发动机爆轰影响实验研究[J].推进技术,2015,36(6): 947-952.ZHENG Quan,WENG Chunsheng,BAI Qiaodong.Experimental study on effects of equivalence ratio on detonation characteristics of liquidfueled rotating detonation engine[J].Journal of Propulsion Technology,2015,36(6): 947-952.
[13]郑权,李宝星,翁春生,等.双波对撞模态下液态燃料旋转爆轰发动机推力测试[J].兵工学报,2017,38(4): 679-689.ZHENG Quan,LI Baoxing WENG Chunsheng,et al.Thrust measurement of liquid-fueled rotating detonation engine under two-wave collision mode[J].Acta Armamentarii,2017,38(4): 679-689.
[14]Deng L,Ma H,Xu C,et al.Investigation on the propagation process of rotating detonation wave[J].Acta Astronautica,2017,139: 278-287.
[15]Kindracki J,Wolanski P,Gut Z.Experimental research on the rotating detonation in gaseous fuels-oxygen mixtures[J].Shock Waves,2011,21(2): 75-84.

更新日期/Last Update: 2019-01-02
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