Investigation into the instability mechanism of hydrogen-oxygen rotating detonation wave propagation using a small-scale model

XU Hongfei; WANG Fang; WU Yuwen; WENG Chunsheng

doi:10.11883/bzycj-2024-0130

Volume 45 Issue 1

Jan. 2025

Turn off MathJax

Article Contents

Abstract

References

Article Navigation > Explosion And Shock Waves > 2025 > 45(1): 012101

WANG De-rong, DAI Ming, LI Jie, WANG Ming-yang. Failure effect of steel-fiber reactive power concrete (RPC) shelter plate under contact explosion[J]. Explosion And Shock Waves, 2008, 28(1): 67-74. doi: 10.11883/1001-1455(2008)01-0067-08

Citation:

XU Hongfei, WANG Fang, WU Yuwen, WENG Chunsheng. Investigation into the instability mechanism of hydrogen-oxygen rotating detonation wave propagation using a small-scale model[J]. Explosion And Shock Waves, 2025, 45(1): 012101. doi: 10.11883/bzycj-2024-0130

Citation:

PDF( 7660 KB)

Investigation into the instability mechanism of hydrogen-oxygen rotating detonation wave propagation using a small-scale model

doi: 10.11883/bzycj-2024-0130

National Key Laboratory of Transient Physics, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China

Received Date: 2024-05-09
Rev Recd Date: 2024-07-12

Available Online: 2024-07-18

Publish Date: 2025-01-01

Abstract

Abstract

The high reactivity of hydrogen and oxygen poses a huge challenge to the stable propagation of rotating detonation waves. To study the propagation instability of hydrogen-oxygen rotating detonation waves, based on the RYrhoCentralFoam solver developed by OpenFOAM, numerical simulations were conducted on two-dimensional hydrogen-oxygen rotating detonation waves in small scale model by changing the equivalence ratio. The complex and variable propagation characteristics of hydrogen-oxygen rotating detonation waves were revealed, and the typical flow field was analyzed. The instability of propagation modes and the quenching and re-initiation mechanisms of detonation waves were explored. The results show that as the equivalence ratio increases, the flow field exhibits three propagation modes: extinction, single wave, and hybrid waves. The detonation wave velocity increases almost linearly with the increase of equivalence ratio, with a velocity deficit of 5% to 8%. The disturbance of shock waves causes significant distortion and wrinkling on the deflagration surface, while the high reactivity of hydrogen and oxygen results in obvious layering on the deflagration surface and different instability at the two interfaces. The upper interface exhibits Kelvin-Helmholtz (K-H) instability, while the lower interface exhibits Rayleigh-Taylor (R-T) instability. As for the hybrid waves, the detonation wave is extremely unstable, maintaining a cycle between three states: quenching, single wave, and double wave collision. There are two ways in which detonation waves can be extinguished: firstly, the collision of two waves leads to the quenching of the detonation wave, and secondly, the intensification of combustion on the deflagration surface leads to the downward movement of the deflagration surface, ultimately resulting in the quenching of the detonation wave. The main reason for re-initiation is that the R-T instability induces detonation products and fresh premixed gas squeezing each other on the deflagration surface. The interaction between fresh premixed gas and products produces spikes and bubbles, enhances the reaction heat release on the deflagration surface, and generates local hotspots. The hotspots gradually increase into detonation waves, achieving the transition from deflagration to detonation.
- rotating detonation wave,
- propagation characteristics,
- equivalence ratio,
- instability,
- quenching and re-initiation

FullText(HTML)

References(37)

References

[1]	LIU Y, ZHOU W J, YANG Y J, et al. Numerical study on the instabilities in H₂-air rotating detonation engines [J]. Physics of Fluids, 2018, 30(4): 046106. DOI: 10.1063/1.5024867.
[2]	MA J Z, LUAN M Y, XIA Z J, et al. Recent progress, development trends, and consideration of continuous detonation engines [J]. AIAA Journal, 2020, 58(12): 4976–5035. DOI: 10.2514/1.J058157.
[3]	VERREAULT J, HIGGINS A J. Initiation of detonation by conical projectiles [J]. Proceedings of the Combustion Institute, 2011, 33(2): 2311–2318. DOI: 10.1016/j.proci.2010.07.086.
[4]	FAN W, YAN C J, HUANG X Q, et al. Experimental investigation on two-phase pulse detonation engine [J]. Combustion and Flame, 2003, 133(4): 441–450. DOI: 10.1016/S0010-2180(03)00043-9.
[5]	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.
[6]	PENG H Y, LIU W D, LIU S J, et al. Hydrogen-air, ethylene-air, and methane-air continuous rotating detonation in the hollow chamber [J]. Energy, 2020, 211: 118598. DOI: 10.1016/j.energy.2020.118598.
[7]	BOHON M D, BLUEMNER R, PASCHEREIT C O, et al. High-speed imaging of wave modes in an RDC [J]. Experimental Thermal and Fluid Science, 2019, 102: 28–37. DOI: 10.1016/j.expthermflusci.2018.10.031.
[8]	吴明亮, 郑权, 续晗, 等. 氢气占比对氢气-煤油-空气旋转爆轰波传播特性的影响 [J]. 兵工学报, 2022, 43(1): 86–97. DOI: 10.3969/j.issn.1000-1093.2022.01.010. WU M L, ZHENG Q, XU H, et al. The influence of hydrogen proportion on the propagation characteristics of hydrogen-kerosene-air rotating detonation waves [J]. Acta Armamentarii, 2022, 43(1): 86–97. DOI: 10.3969/j.issn.1000-1093.2022.01.010.
[9]	张允祯, 程杪, 荣光耀, 等. 低频爆轰不稳定性形成机理的数值模拟研究 [J]. 爆炸与冲击, 2021, 41(9): 092101. DOI: 10.11883/bzycj-2020-0239. ZHANG Y Z, CHENG M, RONG G Y, et al. Numerical investigation on formation mechanism of low-frequency detonation instability [J]. Explosion and Shock Waves, 2021, 41(9): 092101. DOI: 10.11883/bzycj-2020-0239.
[10]	杨帆, 姜春雪, 王宇辉, 等. 煤油液滴直径对两相旋转爆轰发动机流场的影响 [J]. 爆炸与冲击, 2023, 43(2): 022101. DOI: 10.11883/bzycj-2022-0068. YANG F, JIANG C X, WANG Y H, et al. Influence of kerosene droplet diameters on the flow field of a two-phase rotating detonation engine [J]. Explosion and Shock Waves, 2023, 43(2): 022101. DOI: 10.11883/bzycj-2022-0068.
[11]	丁陈伟, 翁春生, 武郁文, 等. 基于液体碳氢燃料的旋转爆轰燃烧特性研究 [J]. 爆炸与冲击, 2022, 42(2): 022101. DOI: 10.11883/bzycj-2021-0065. DING C W, WENG C S, WU Y W, et al. Combustion characteristics of rotating detonation based on liquid hydrocarbon fuel [J]. Explosion and Shock Waves, 2022, 42(2): 022101. DOI: 10.11883/bzycj-2021-0065.
[12]	张树杰, 张立锋, 姚松柏, 等. 当量比对连续旋转爆轰发动机的影响研究 [J]. 兵工学报, 2017, 38(S1): 1–7. ZHANG S J, ZHANG L F, YAO S B, et al. Numerical investigation on rotating detonation engine with varying equivalence ratios [J]. Acta Armamentarii, 2017, 38(S1): 1–7.
[13]	孟庆洋, 赵宁波, 郑洪涛, 等. 非预混条件下的旋转爆轰燃烧室双波头演化过程数值模拟 [J]. 航空动力学报, 2019, 34(1): 51–62. DOI: 10.13224/j.cnki.jasp.2019.01.007. MENG Q Y, ZHAO N B, ZHENG H T, et al. Numerical study on the two-wave transition process in rotating detonation combustor under separate injection condition [J]. Journal of Aerospace Power, 2019, 34(1): 51–62. DOI: 10.13224/j.cnki.jasp.2019.01.007.
[14]	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.
[15]	FAN L Z, SHI Q, ZHI Y, et al. Experimental and numerical study on multi-wave modes of H₂/O₂ rotating detonation combustor [J]. International Journal of Hydrogen Energy, 2022, 47(26): 13121–13133. DOI: 10.1016/j.ijhydene.2022.02.048.
[16]	ANAND V, ST. GEORGE A, DRISCOLL R, et al. Characterization of instabilities in a Rotating Detonation Combustor [J]. International Journal of Hydrogen Energy, 2015, 40(46): 16649–16659. DOI: 10.1016/j.ijhydene.2015.09.046.
[17]	HISHIDA M, FUJIWARA T, WOLANSKI P. Fundamentals of rotating detonations [J]. Shock Waves, 2009, 19(1): 1–10. DOI: 10.1007/s00193-008-0178-2.
[18]	LI Q, LIU P X, ZHANG H X. Further investigations on the interface instability between fresh injections and burnt products in 2-D rotating detonation [J]. Computers & Fluids, 2018, 170: 261–272. DOI: 10.1016/j.compfluid.2018.05.005.
[19]	LIU P X, LI Q, HUANG Z F, et al. Interpretation of wake instability at slip line in rotating detonation [J]. International Journal of Computational Fluid Dynamics, 2018, 32(8/9): 379–394. DOI: 10.1080/10618562.2018.1533634.
[20]	ZHAO M J, LI J M, TEO C J, et al. Effects of variable total pressures on instability and extinction of rotating detonation combustion [J]. Flow, Turbulence and Combustion, 2020, 104(1): 261–290. DOI: 10.1007/s10494-019-00050-y.
[21]	STECHMANN D P. Experimental study of high-pressure rotating detonation combustion in rocket environments [D]. West Lafayette: Purdue University, 2017.
[22]	WANG Y H, WANG J P. Coexistence of detonation with deflagration in rotating detonation engines [J]. International Journal of Hydrogen Energy, 2016, 41(32): 14302–14309. DOI: 10.1016/j.ijhydene.2016.06.026.
[23]	BYKOVSKII F A, ZHDAN S A, VEDERNIKOV E F, et al. Continuous detonation of a hydrogen-oxygen gas mixture in a 100-mm plane-radial combustor with exhaustion toward the periphery [J]. Shock Waves, 2020, 30(3): 235–243. DOI: 10.1007/s00193-019-00919-x.
[24]	BYKOVSKII F A, ZHDAN S A, VEDERNIKOV E F, et al. Detonation combustion of a hydrogen–oxygen mixture in a plane–radial combustor with exhaustion toward the center [J]. Combustion, Explosion, and Shock Waves, 2016, 52(4): 446–456. DOI: 10.1134/s0010508216040080.
[25]	KELLER P K, POLANKA M D, SCHAUER F R, et al. Low mass-flow operation of small-scale rotating detonation engine [J]. Applied Thermal Engineering, 2024, 241: 122352. DOI: 10.1016/j.applthermaleng.2024.122352.
[26]	HUANG Z W, ZHAO M J, XU Y, et al. Eulerian-Lagrangian modelling of detonative combustion in two-phase gas-droplet mixtures with OpenFOAM: validations and verifications [J]. Fuel, 2021, 286: 119402. DOI: 10.1016/j.fuel.2020.119402.
[27]	ZHANG H W, ZHAO M J, HUANG Z W. Large eddy simulation of turbulent supersonic hydrogen flames with OpenFOAM [J]. Fuel, 2020, 282: 118812. DOI: 10.1016/j.fuel.2020.118812.
[28]	CONAIRE M Ó, CURRAN H J, SIMMIE J M, et al. A comprehensive modeling study of hydrogen oxidation [J]. International Journal of Chemical Kinetics, 2004, 36(11): 603–622. DOI: 10.1002/kin.20036.
[29]	LIU X Y, LUAN M Y, CHEN Y L, et al. Flow-field analysis and pressure gain estimation of a rotating detonation engine with banded distribution of reactants [J]. International Journal of Hydrogen Energy, 2020, 45(38): 19976–19988. DOI: 10.1016/j.ijhydene.2020.05.102.
[30]	BENGOECHEA S, REISS J, LEMKE M, et al. Adjoint-based optimisation of detonation initiation by a focusing shock wave [J]. Shock Waves, 2021, 31(7): 789–805. DOI: 10.1007/s00193-020-00973-w.
[31]	RUDY W, ZBIKOWSKI M, TEODORCZYK A. Detonations in hydrogen-methane-air mixtures in semi confined flat channels [J]. Energy, 2016, 116: 1479–1483. DOI: 10.1016/j.energy.2016.06.001.
[32]	RUDY W, KUZNETSOV M, POROWSKI R, et al. Critical conditions of hydrogen-air detonation in partially confined geometry [J]. Proceedings of the Combustion Institute, 2013, 34(2): 1965–1972. DOI: 10.1016/j.proci.2012.07.019.
[33]	WANG F, WENG C S, ZHANG H W. Semi-confined layered kerosene/air two-phase detonations bounded by nitrogen gas [J]. Combustion and Flame, 2023, 258: 113104. DOI: 10.1016/j.combustflame.2023.113104.
[34]	ZHANG S, YAO S, LUAN M, et al. Effects of injection conditions on the stability of rotating detonation waves [J]. Shock Waves, 2018, 28(5): 1079–1087. DOI: 10.1007/s00193-018-0854-9.
[35]	GOODWIN G B, ORAN E S. Premixed flame stability and transition to detonation in a supersonic combustor [J]. Combustion and Flame, 2018, 197: 145–160. DOI: 10.1016/j.combustflame.2018.07.008.
[36]	MENG Q Y, ZHAO M J, ZHENG H T, et al. Eulerian-Lagrangian modelling of rotating detonative combustion in partially pre-vaporized n-heptane sprays with hydrogen addition [J]. Fuel, 2021, 290: 119808. DOI: 10.1016/j.fuel.2020.119808.
[37]	GEORGE A C S, DRISCOLL R B, ANAND V, et al. Starting transients and detonation onset behavior in a rotating detonation combustor [C]//Proceedings of the 54th AIAA Aerospace Sciences Meeting. San Diego: AIAA, 2016. DOI: 10.2514/6.2016-0126.

Relative Articles

[1]	ZHOU Dezheng, LI Xiaojie, WANG Xiaohong, WANG Yuxin, YAN Honghao. Analysis of internal load and dynamic response of vacuum explosion containment vessel with sand covered for explosive welding[J]. Explosion And Shock Waves, 2024, 44(10): 101407. doi: 10.11883/bzycj-2023-0455
[2]	WEI Xiao, CHENG Yangfan, ZHU Rongkang, SUN Renhao, WANG Quan. Explosion characteristics and thermal safety of low detonation velocity emulsion explosives containing coal-based solid waste fly ash microspheres[J]. Explosion And Shock Waves. doi: 10.11883/bzycj-2024-0117
[3]	LI Rui, LI Xiaochen, WANG Quan, YUAN Yuhong, HONG Xiaowen, HUANG Yinsheng. Propagation characteristics of blast wave in diminished ambient temperature and pressure environments[J]. Explosion And Shock Waves, 2023, 43(2): 022301. doi: 10.11883/bzycj-2022-0188
[4]	XU Weizheng, HUANG Chao, ZHANG Pan, HUANG Yu, ZENG Fan, WANG Xing, ZHENG Xianxu. A method for calculating underwater explosion shock wave parameters of slender cone-shaped charges[J]. Explosion And Shock Waves, 2022, 42(1): 014203. doi: 10.11883/bzycj-2021-0095
[5]	ZHANG Qiwei, CHENG Yangfan, XIA Yu, WANG Zhonghua, WANG Quan, SHEN Zhaowu. Application of colorimetric pyrometer in the measurement of transient explosion temperature[J]. Explosion And Shock Waves, 2022, 42(11): 114101. doi: 10.11883/bzycj-2021-0477
[6]	LI Xuejiao, WU Yong, WANG Qi, GAO Yugang, WANG Quan, WANG Yixin, MA Honghao. Study on energy output characteristics of underwater explosion of energetic microballoon sensitized emulsion explosive[J]. Explosion And Shock Waves, 2022, 42(3): 032301. doi: 10.11883/bzycj-2021-0188
[7]	NIE Yuan, JIANG Jianwei, MEN Jianbing. Calculation models for parameters of spherical charge blasting shock wave considering ambient temperature and humidity[J]. Explosion And Shock Waves, 2018, 38(4): 735-742. doi: 10.11883/bzycj-2016-0340
[8]	Cheng Yang-fan, Ma Hong-hao, Shen Zhao-wu. Experimental research on pressure desensitization of emulsion explosive sensitized by MgH₂[J]. Explosion And Shock Waves, 2014, 34(4): 427-432. doi: 10.11883/1001-1455(2014)04-0427-06
[9]	WANG Xiao-hong, LI Xiao-jie, YAN Hong-hao, YI Cai-hong, LUO Ning. Detonationreactioncharacteristicofemulsionexplosives usedfornano-materialssynthesi[J]. Explosion And Shock Waves, 2012, 32(5): 523-527. doi: 10.11883/1001-1455(2012)05-0523-05
[10]	ZHANG Yu-lei, NI Ou-qi, HOU Kuang-yi, LI Bin, ZHU Ying-zhong, HAN Zhi-we. Experimentalstudyonemulsionexplosivescharged intothecurvedgrooveinanironplate[J]. Explosion And Shock Waves, 2012, 32(2): 216-220. doi: 10.11883/1001-1455(2012)02-0216-05
[11]	WANG Yin-Jun, LI Yu-Jing, GAN De-Huai. Pressure desensitization of emulsion explosives sensitized by compound sensitizers[J]. Explosion And Shock Waves, 2010, 30(3): 308-313. doi: 10.11883/1001-1455(2010)03-0308-06
[12]	LI Jin-he, ZHAO Ji-bo, TAN Duo-wang, WANG Yan-ping, ZHANG Yuan-ping. Underwater shock wave performances of explosives[J]. Explosion And Shock Waves, 2009, 29(2): 172-176. doi: 10.11883/1001-1455(2009)02-0172-05
[13]	LI Jia-bo, ZHOU Xian-ming, WANG Xiang. A fast pyrometer with wide dynamic linearity for shock temperature measurements[J]. Explosion And Shock Waves, 2009, 29(6): 625-631. doi: 10.11883/1001-1455(2009)06-0625-07
[14]	WANG Yin-jun, LI Jin-jun, FANG Hong. Influences of emulsion explosive density on its pressure desensitization[J]. Explosion And Shock Waves, 2009, 29(5): 529-534. doi: 10.11883/1001-1455(2009)05-0529-06
[15]	YAN Shi-long, WANG Yin-jun. Characterization of pressure desensitization of emulsion explosive subjected to shock wave[J]. Explosion And Shock Waves, 2006, 26(5): 441-447. doi: 10.11883/1001-1455(2006)05-0441-07

Supplements(0)

Cited By

Cited by

Periodical cited type(2)

1.	鲜鹏，李军. 喷丸技术的发展与研究. 金属世界. 2020(01): 32-36 .
2.	董星，刘雨庆，段雄. 前混合水射流多弹丸喷丸模型及残余应力场的数值模拟. 机械工程学报. 2020(04): 224-232 .