Citation: | WANG Shunli, WU Yun, JIN Di, GUO Shanguang, ZHONG Yepan, YANG Xingkui. Effects of nozzles on performance of rotating detonation at different equivalence ratios[J]. Explosion And Shock Waves, 2020, 40(10): 102102. doi: 10.11883/bzycj-2019-0481 |
[1] |
VOITSEKHOVSKⅡ B V. Maintained detonations [J]. Soviet Physics Doklady, 1960, 4(6): 1207–1209.
|
[2] |
BYKOVSKⅡ F A, MITROFANOV V V. Detonation combustion of a gas mixture in a cylindrical chamber [J]. Combustion, Explosion and Shock Waves, 1980, 16(5): 570–578. DOI: 10.1007/BF00794937.
|
[3] |
BYKOVSKⅡ F A, ZHDAN S A, VEDERNIKOV E F. Spin detonation of fuel-air mixtures in a cylindrical combustor [J]. Doklady Physics, 2005, 50(1): 56–58. DOI: 10.1134/1.1862376.
|
[4] |
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.
|
[5] |
BYKOVSKⅡ F A, ZHDAN S A, VEDERNIKOV E F. Continuous spin detonation of hydrogen-oxygen mixtures: 1: annular cylindrical combustors [J]. Combustion, Explosion, and Shock Waves, 2008, 44(2): 150–162. DOI: 10.1007/s10573-008-0021-1.
|
[6] |
BYKOVSKⅡ F A, ZHDAN S A, VEDERNIKOV E F. Continuous spin detonation of hydrogen-oxygen mixtures: 2: combustor with an expanding annular channel [J]. Combustion, Explosion, and Shock Waves, 2008, 44(3): 330–342. DOI: 10.1007/s10573-008-0041-x.
|
[7] |
LU F K, BRAUN E M. Rotating detonation wave propulsion: experimental challenges, modeling, and engine concepts [J]. Journal of Propulsion and Power, 2014, 30(5): 1125–1142. DOI: 10.2514/1.B34802.
|
[8] |
WOLAŃSKI P. Detonative propulsion [J]. Proceedings of the Combustion Institute, 2013, 34(1): 125–158. DOI: 10.1016/j.proci.2012.10.005.
|
[9] |
SHAO Y T, LIU M, WANG J P. Continuous detonation engine and effects of different types of nozzle on its propulsion performance [J]. Chinese Journal of Aeronautics, 2010, 23(6): 647–652. DOI: 10.1016/s1000-9361(09)60266-1.
|
[10] |
YI T H, LOU J, TURANGAN C, et al. Effect of nozzle shapes on the performance of continuously-rotating detonation engine [C] // Proceedings of the 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando: AIAA, 2010. DOI: 10.2514/6.2010-152.
|
[11] |
JOURDAINE N, TSUBOI N, OZAWA K, et al. Three-dimensional numerical thrust performance analysis of hydrogen fuel mixture rotating detonation engine with aerospike nozzle [J]. Proceedings of the Combustion Institute, 2019, 37(3): 3443–3451. DOI: 10.1016/j.proci.2018.09.024.
|
[12] |
KATO Y, ISHIHARA K, MATSUOKA K, et al. Study of combustion chamber characteristic length in rotating detonation engine with convergent-divergent nozzle [C] // Proceedings of the 54th AIAA Aerospace Sciences Meeting. San Diego: AIAA, 2016. DOI: 10.2514/6.2016-1406.
|
[13] |
高剑, 马虎, 裴晨曦, 等. 喷管对旋转爆震发动机性能影响的实验 [J]. 航空动力学报, 2016, 31(10): 2443–2453. DOI: 10.13224/j.cnki.jasp.2016.10.018.
GAO J, MA H, PEI C X, et al. Experiment of effect of nozzle shapes on the performance of rotating detonation engine [J]. Journal of Aerospace Power, 2016, 31(10): 2443–2453. DOI: 10.13224/j.cnki.jasp.2016.10.018.
|
[14] |
FOTIA M, KAEMMING T A, CODONI J R, et al. Experimental thrust sensitivity of a rotating detonation engine to various aerospike plug-nozzle configurations [C] // Proceedings of AIAA Scitech 2019 Forum. San Diego: AIAA, 2019. DOI: 10.2514/6.2019-1743.
|
[15] |
RANKIN B A, HOKE J, SCHAUER F. Periodic exhaust flow through a converging-diverging nozzle downstream of a rotating detonation engine [C] // Proceedings of the 52nd Aerospace Sciences Meeting. National Harbor: AIAA, 2014. DOI: 10.2514/6.2014-1015.
|
[16] |
SONG F L, WU Y, XU S D, et al. Pre-combustion cracking characteristics of kerosene [J]. Chemical Physics Letters, 2019, 737: 136812. DOI: 10.1016/j.cplett.2019.136812.
|
[17] |
SONG F L, WU Y, XU S D, et al. Effects of refueling position and residence time on pre-combustion cracking characteristic of aviation kerosene RP-3 [J]. Fuel, 2020, 270: 117548. DOI: 10.1016/j.fuel.2020.117548.
|
[18] |
BLUEMNER R, BOHON M, PASCHEREIT C O, et al. Dynamics of counter-rotating wave modes in an RDC [C] // Proceedings of 2018 Joint Propulsion Conference. Cincinnati: AIAA, 2018. DOI: 10.2514/6.2018-4572.
|
[19] |
刘世杰, 林志勇, 刘卫东, 等. 连续旋转爆震波传播过程研究:Ⅱ: 双波对撞传播模式 [J]. 推进技术, 2014, 35(2): 269–275. DOI: 10.13675/j.cnki.tjjs.2014.02.031.
LIU S J, LIN Z Y, LIU W D, et al. Research on continuous rotating detonation wave propagation process: Ⅱ: two-wave collision propagation mode [J]. Journal of Propulsion Technology, 2014, 35(2): 269–275. DOI: 10.13675/j.cnki.tjjs.2014.02.031.
|
[20] |
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.
|
[21] |
ZHONG Y P, WU Y, JIN D, et al. Investigation of rotating detonation fueled by the pre-combustion cracked kerosene [J]. Aerospace Science and Technology, 2019, 95: 105480. DOI: 10.1016/j.ast.2019.105480.
|