Citation: | GE Gaoyang, MA Yuan, HOU Shizhuo, XIA Zhenjuan, MA Hu, DENG Li, ZHOU Changsheng. Experimental study on the effect of equivalent ratio on working characteristics of gasoline fuel two-phase rotating detonation engine[J]. Explosion And Shock Waves, 2021, 41(11): 112102. doi: 10.11883/bzycj-2020-0465 |
[1] |
BYKOVSKII F A, MITROFANOV V V, VEDERNIKOV E F. Continuous detonation combustion of fuel-air mixtures [J]. Combustion, Explosion and Shock Waves, 1997, 33(3): 344–353. DOI: 10.1007/BF02671875.
|
[2] |
BYKOVSKII F A, ZHDAN S A, VEDERNIKOV E F. Continuous spin detonation of fuel-air mixtures [J]. Combustion, Explosion and Shock Waves, 2006, 42(4): 463–471. DOI: 10.1007/s10573-006-0076-9.
|
[3] |
BYKOVSKII F A, ZHDAN S A, VEDERNIKOV E F. Continuous spin detonations [J]. Journal of Propulsion and Power, 2006, 22(6): 1204–1216. DOI: 10.2514/1.17656.
|
[4] |
BYKOVSKII F A, ZHDAN S A, VEDERNIKOV E F. Initiation of detonation of fuel-air mixtures in a flow-type annular combustor [J]. Combustion, Explosion, and Shock Waves, 2014, 50(2): 214–222. DOI: 10.1134/S0010508214020130.
|
[5] |
BYKOVSKII F A, ZHDAN S A, VEDERNIKOV E F. Continuous spin detonation of a heterogeneous kerosene-air mixture with addition of hydrogen [J]. Combustion, Explosion, and Shock Waves, 2016, 52(3): 371–373. DOI: 10.1134/S0010508216030187.
|
[6] |
BYKOVSKII F A, ZHDAN S A, VEDERNIKOV E F. Continuous detonation of the liquid kerosene-air mixture with addition of hydrogen or syngas [J]. Combustion, Explosion, and Shock Waves, 2019, 55(5): 589–598. DOI: 10.1134/S0010508219050101.
|
[7] |
FROLOV S M, AKSENOV V S, IVANOV V S, et al. Continuous detonation combustion of ternary “hydrogen-liquid propane-air” mixture in annular combustor [J]. International Journal of Hydrogen Energy, 2017, 42(26): 16808–16820. DOI: 10.1016/j.ijhydene.2017.05.138.
|
[8] |
KINDRACKI J. Experimental studies of kerosene injection into a model of a detonation chamber [J]. Journal of Power Technologies, 2012, 92(2): 80–89.
|
[9] |
KINDRACKI J. Study of detonation initiation in kerosene-oxidizer mixtures in short tubes [J]. Shock Waves, 2014, 24(6): 603–618. DOI: 10.1007/s00193-014-0519-2.
|
[10] |
KINDRACKI J. Experimental research on rotating detonation in liquid fuel-gaseous air mixtures [J]. Aerospace Science and Technology, 2015, 43: 445–453. DOI: 10.1016/j.ast.2015.04.006.
|
[11] |
LIU Y S, WANG Y H, LI Y S, et al. Spectral analysis and self-adjusting mechanism for oscillation phenomenon in hydrogen-oxygen continuously rotating detonation engine [J]. Chinese Journal of Aeronautics, 2015, 28(3): 669–675. DOI: 10.1016/j.cja.2015.03.006.
|
[12] |
XIE Q F, WEN H C, LI W H, et al. Analysis of operating diagram for H2/Air rotating detonation combustors under lean fuel condition [J]. Energy, 2018, 151: 408–419. DOI: 10.1016/j.energy.2018.03.062.
|
[13] |
LIN W, ZHOU J, LIU S J, et al. Experimental study on propagation mode of H2/Air continuously rotating detonation wave [J]. International Journal of Hydrogen Energy, 2015, 40(4): 1980–1993. DOI: 10.1016/j.ijhydene.2014.11.119.
|
[14] |
魏万里, 翁春生, 武郁文, 等. 氧化剂喷注面积对连续旋转爆轰波传播特性影响的实验研究 [J]. 兵工学报, 2018, 39(12): 2345–2353. DOI: 10.3969/j.issn.1000-1093.2018.12.008.
WEI W L, WENG C S, WU Y W, et al. Experimental research on influence of oxidant injection area on the propagation characteristics of continuous rotating detonation wave [J]. Acta Armamentarii, 2018, 39(12): 2345–2353. DOI: 10.3969/j.issn.1000-1093.2018.12.008.
|
[15] |
DENG L, MA H, XU C, et al. The feasibility of mode control in rotating detonation engine [J]. Applied Thermal Engineering, 2018, 129: 1538–1550. DOI: 10.1016/j.applthermaleng.2017.10.146.
|
[16] |
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. DOI: 10.13675/j.cnki.tjjs.2015.06.020.
ZHENG Q, WENG C S, BAI Q D. 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. DOI: 10.13675/j.cnki.tjjs.2015.06.020.
|
[17] |
郑权, 李宝星, 翁春生, 等. 双波对撞模态下的液态燃料旋转爆轰发动机推力测试研究 [J]. 兵工学报, 2017, 38(4): 679–689. DOI: 10.3969/j.issn.1000-1093.2017.04.008.
ZHENG Q, LI B X, WENG C S, et al. Thrust measurement of liquid-fueled rotating detonation engine under two-wave collision mode [J]. Acta Armamentarii, 2017, 38(4): 679–689. DOI: 10.3969/j.issn.1000-1093.2017.04.008.
|
[18] |
李宝星, 王中, 许桂阳, 等. 煤油燃料旋转爆轰波起爆与传播特性实验研究 [J]. 兵工学报, 2020, 41(7): 1339–1346. DOI: 10.3969/j.issn.1000-1093.2020.07.011.
LI B X, WANG Z, XU G Y, et al. Experimental research on initiation and propagation characteristics of kerosene fuel rotating detonation wave [J]. Acta Armamentarii, 2020, 41(7): 1339–1346. DOI: 10.3969/j.issn.1000-1093.2020.07.011.
|
[19] |
王迪, 周进, 林志勇. 煤油两相连续旋转爆震燃烧室工作特性试验研究 [J]. 推进技术, 2017, 38(2): 471–480. DOI: 10.13675/j.cnki.tjjs.2017.02.028.
WANG D, ZHOU J, LIN Z Y. Experimental investigation on operating characteristics of two-phase continuous rotating detonation combustor fueled by kerosene [J]. Journal of Propulsion Technology, 2017, 38(2): 471–480. DOI: 10.13675/j.cnki.tjjs.2017.02.028.
|