Effect of transversal concentration gradient on H2-O2 cellular detonation

doi:10.1088/1674-1056/ab81f5

中国物理B ›› 2020, Vol. 29 ›› Issue (6): 60503-060503.doi: 10.1088/1674-1056/ab81f5

• SPECIAL TOPIC—Recent advances in thermoelectric materials and devices • 上一篇下一篇

Effect of transversal concentration gradient on H₂-O₂ cellular detonation

Cheng Wang(王成), Yi-Xuan Wu(吴易烜), Jin Huang(黄金), Wen-Hu Han(韩文虎), Qing-Guan Song(宋清官)

1 State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing 100081, China;
2 Institute of Chemical Materials, China Academy of Engineering Physics, Mianyang 621900, China

收稿日期:2019-11-18 修回日期:2020-03-09 出版日期:2020-06-05 发布日期:2020-06-05
通讯作者: Jin Huang E-mail:huangjin@bit.edu.cn
基金资助:
Project supported by the Natural National Science Foundation of China (Grant Nos. 11972090, 11732003, and U1830139), the Beijing Natural Science Foundation, China (Grant No. 8182050), and the National Key Research and Development Program of China (Grant No. 2017YFC0804700).

Effect of transversal concentration gradient on H₂-O₂ cellular detonation

Cheng Wang(王成)¹, Yi-Xuan Wu(吴易烜)¹, Jin Huang(黄金)¹, Wen-Hu Han(韩文虎)¹, Qing-Guan Song(宋清官)²

1 State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing 100081, China;
2 Institute of Chemical Materials, China Academy of Engineering Physics, Mianyang 621900, China

Received:2019-11-18 Revised:2020-03-09 Online:2020-06-05 Published:2020-06-05
Contact: Jin Huang E-mail:huangjin@bit.edu.cn
Supported by:
Project supported by the Natural National Science Foundation of China (Grant Nos. 11972090, 11732003, and U1830139), the Beijing Natural Science Foundation, China (Grant No. 8182050), and the National Key Research and Development Program of China (Grant No. 2017YFC0804700).

摘要/Abstract

摘要：

A two-dimensional detonation in H₂-O₂ system is simulated by a high-resolution code based on the fifth-order weighted essentially non-oscillatory (WENO) scheme in the spatial discretization and the 3th-order additive Runge-Kutta schemes in the time discretization, by using a detailed chemical model. The effect of a concentration gradient on cellular detonation is investigated. The results show that with the increase of the concentration gradient, the cell instability of detonation increases and gives rise to the oscillation of average detonation velocity. After a long time, for the case of the lower gradient the detonation can be sustained, with the multi-head mode and single-head mode alternating, while for the higher gradient it propagates with a single-head mode.

关键词: detonation, detailed reaction, WENO, additive Runge-Kutta (ARK), concentration gradient

Abstract:

Key words: detonation, detailed reaction, WENO, additive Runge-Kutta (ARK), concentration gradient

中图分类号: (Thermodynamics)

05.70.-a

45.20.dh (Energy conservation) 47.10.ad (Navier-Stokes equations) 47.40.Rs (Detonation waves)

王成, 吴易烜, 黄金, 韩文虎, 宋清官. Effect of transversal concentration gradient on H₂-O₂ cellular detonation[J]. 中国物理B, 2020, 29(6): 60503-060503.

Cheng Wang(王成), Yi-Xuan Wu(吴易烜), Jin Huang(黄金), Wen-Hu Han(韩文虎), Qing-Guan Song(宋清官). Effect of transversal concentration gradient on H₂-O₂ cellular detonation[J]. Chin. Phys. B, 2020, 29(6): 60503-060503.

参考文献 33

[1]	Liu J C, Liou J J, Sichel M, Kauffman C W and Nicholls J A 1988 21th Symposium (International) on Combustion, August 3-8, 1988, Technical University of Munich West Germany, Munich, Germany, pp. 1639-1647
[2]	Short M and Sharpe G J 2003 Combust. Thoer. Model. 7 401 doi: 10.1088/1364-7830/7/2/311
[3]	Short M 2001 J. Fluid Mech. 430 381 doi: 10.1017/S0022112000003116
[4]	Ng H D, Radulescu M I, Higgins A J, Nikiforakis N and Lee J H S 2005 Combust. Theor. Model. 9 385 doi: 10.1080/13647830500307758
[5]	Zhang B, Liu H, Yan B J and Ng H D 2020 Fuel 259 116220 doi: 10.1016/j.fuel.2019.116220
[6]	Zhang B 2019 Fuel 253 305 doi: 10.1016/j.fuel.2019.05.006
[7]	Zhang B and Liu H 2019 Fuel 258 116132 doi: 10.1016/j.fuel.2019.116132
[8]	Lieberman D H and Shepherd J E 2007 Shock Waves 16 421 doi: 10.1007/s00193-007-0080-3
[9]	Bull D C, Elsworth J E, McLeod M A and Hughes D 1981 Prog. Astronaut. Aeronaut. 75 61
[10]	Donato M, Donato L and Lee J H 1981 Proceedings of the First Specialists Meeting of the Combustion Institute, July 20-25, 1981, Bordeaux, France
[11]	Li J, Lai W H, Chung K and Lu F K 2008 Combust. Flame 154 331 doi: 10.1016/j.combustflame.2008.04.010
[12]	Ishii K and Kojima M 2007 Shock Waves 17 95 doi: 10.1007/s00193-007-0093-y
[13]	Thomas G O, Sutton P and Edwards D H 1991 Combust. Flame 84 312 doi: 10.1016/0010-2180(91)90008-Y
[14]	Vidal P 2009 Int. J. Spray Combust 1 435 doi: 10.1260/175682709789685822
[15]	Oran E S, Jones D A and Sichel M 1992 P. Roy. Soc. A-Math. Phys. 436 267
[16]	Vollmer K G, Ettner F and Sattelmayer T 2012 Combust. Sci. Technol. 184 1903 doi: 10.1080/00102202.2012.690652
[17]	Kessler D A, Gamezo V N and Oran E S 2011 Proceedings of the 23th International Colloquium on the Dynamics of Explosions and Reacting Systems, July 24-29, 2011, Irvine, California, USA
[18]	Boeck L R, Berger F M, Hasslberger J and Settalmayer T 2016 Shock Waves 26 181 doi: 10.1007/s00193-015-0598-8
[19]	Ishii K and Kojima M 2007 Shock Waves 1 795
[20]	Calhoon W H Jr and Sinha N 2005 43rd AIAA Aerospace Sciences Meeting and Exhibit, January 10-13, 2005, Reno, Navada, USA, pp. 42-43
[21]	Kessler D A, Gamezo V N and Oran E S 2011 Proc. Roy. Soc. A-Math. Phys. 370 567
[22]	Ettner F, Vollmer K G and Sattelmayer T 2010 Proceedings of the 8th International Symposium on Hazards, Prevention and Mitigation of Industrial Explosions, September 5-10, 2010, Yokohama, Japan
[23]	Berets D J, Greene E F and Kistiakowsky G B 1950 J. Am. Chem. Soc. 72 1080 doi: 10.1021/ja01159a008
[24]	Engebretsen T, Bjerketvedt D and Sonju O K 1992 Prog. Astronaut. Aeronaut. 153 324
[25]	Kuznetsov M S, Dorofeev S B, Efimenko A A, Alekseev V I and Breitung W 1997 Shock Waves 7 297 doi: 10.1007/s001930050084
[26]	Kuznetsov M, Alekseev V I, Dorofeev S, Matsukov I D and Boccio J L 1998 P. Combust. Inst. 27 2241 doi: 10.1016/S0082-0784(98)80073-8
[27]	Qu Q, Khoo B C, Dou H S and Tsai H M 2008 Shock Waves 18 213 doi: 10.1007/s00193-008-0157-7
[28]	Sánchez A L and Williams F A 2014 Prog. Energy Combust. Sci. 41 1
[29]	Sochet I, Lamy T and Brossard J 2000 Shock Waves 10 363 doi: 10.1007/s001930000066
[30]	Sánchez A L and Williams F A 2014 Prog. Energy Combust. Sci. 41 1
[31]	Tonello N A, Sichel M and Kauffman C W 1995 Shock Waves 5 225 doi: 10.1007/BF01419004
[32]	Huang J, Han W H, Gao X Y and Wang C 2019 Chin. Phys. B 28 074704 doi: 10.1088/1674-1056/28/7/074704
[33]	Austin J M, Pintgen F and Shepherd J E 2004 42nd AIAA Aerospace Sciences Meeting and Exhibit, January 5-8, 2004, Reno, Nevada

Effect of transversal concentration gradient on H₂-O₂ cellular detonation

Effect of transversal concentration gradient on H₂-O₂ cellular detonation

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