[1] 王建平,周蕊,武丹. 连续旋转爆轰发动机的研究进展[J].实验流体力学,2015,29(4):12-25. WANG J P, ZHOU R, WU D. Progress of continuously rotating detonation engine research[J]. Journal of Experiments in Fluid Mechanics, 2015, 29(4):12-25. (in Chinese) [2] BYKOVSKII F A, ZHDAN S A, ADERNIKOV E F. Continuous spin detonation in annular combustors[J]. Combustion, Explosion and Shock Waves, 2005,41(4):449-459. [3] BYKOVSKII F A, ZHDAN S A, ADERNIKOV E F. Continuous spin detonation of fuel-air mixtures [J]. Combustion, Explosion, and Shock Waves, 2006, 42(4):463-471 [4] BYKOVSKII F A, ZHDAN S A, ADERNIKOV E F. Continuous spin detonation of hydrogen-oxygen mixture. 1. annular cylindrical combustor[J]. Combustion, Explosion, and Shock Waves, 2008, 44(2):150-162 [5] 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. [6] KINDRACKI J. Experimental research on rotating detonation in liquid fuel-gaseous air mixtures[J]. Aerospace Science and Technology, 2015, 43:445-453. [7] FRANCOIS F, BRUNO L N. MBDA R&T effort on pulsed and continuous detonation wave engines[J]. Transactions of Nanjing University of Aeronautics & Astronautics, 2011, 28(1):2583-2589. [8] 何煦虹.MBDA公布英仙座超声速导弹系统概念[J]. 飞航导弹, 2012(2): 3-6. HE X H. MBDA announces the concept of Perseus supersonic missile system[J]. Winged Missiles Journal, 2012(2): 3-6.(in Chinese) [9] LIU Y S, WANG Y H, LI Y S, et al. Spectral analysis and self-adjusting mechanism for oscillation phenomenon in H2/O2 continuously rotating detonation engine[J]. Chinese Journal of Aeronautics, 2015, 28(3): 669-675.
[10] 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. [11] 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: 国防科学技术大学, 2012. LIU S J. Investigation on the structure, rotating mode and mechanism of continuous rotating detonation wave[D]. Changsha: National University of Defense Technology, 2012.(in Chinese) [12] 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. [13] PENG H Y, LIU W D, LIU S J, et al. The effect of cavity on ethylene-air continuous rotating detonation in the annular combustor[J]. International Journal of Hydrogen Energy, 2019,44(26): 14032-14043. [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. 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.(in Chinese) [15] 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. ZHENG Q, WENG C S, BAI Q D. Experiment on continuous rotating detonation engine with tilt slot injector[J]. Journal of Propulsion Technology, 2014, 35(4):570-576.(in Chinese) [16] 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. [17] ZHOU S B, MA H, CHEN S H, et al. Experimental investigation on propagation characteristics of rotating detonation wave with a hydrogen-ethylene-acetylene fuel[J]. Acta Astronautica, 2019, 157: 310-320. [18] 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. WANG D, ZHOU J, LIN Z Y. Experimental investigation on operation characteristics of two-phase continuous rotating detonation combustor fueled by kerosene[J]. Journal of Propulsion Techno- logy, 2017, 38(2):471-480.(in Chinese) [19] 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 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. (in Chinese) [20] 李宝星, 翁春生. 连续旋转爆轰发动机气液两相爆轰波传播特性二维数值研究[J]. 固体火箭技术, 2015, 38(5):646-652. LI B X, WENG C S. Numerical investigation on two-dimensional gas-liquid two-phase detonation wave propagation characteristics of continuous rotating detonation engine[J]. Journal of Solid Rocket Technology, 2015, 38(5):646-652.(in Chinese) [21] 李宝星,翁春生.气体与液体两相连续旋转爆轰发动机爆轰被传播特性三维数值模拟研究[J].兵工学报,2017,38(7):1358-1367. LI B X, WENG C S. Three-dimensional numerical simulation on the propagation characteristics of detonation wave in gas-liquid two-phase continuous rotating detonation engine[J]. Acta Armamentarii, 2017,38(7):1358-1367. (in Chinese)
第41卷第7期2020 年7月 兵工学报ACTA ARMAMENTARII Vol.41No.7Jul.2020
|