Quantitative experimental study on detonation instability of multi-component

被引:0
作者
Zhao, Huanjuan [1 ,2 ]
Bao, Yingxin [1 ]
Yu, Kang [2 ]
Liu, Jing [1 ]
Qian, Xinming [3 ]
机构
[1] College of Civil and Resource Engineering, University of Science and Technology Beijing, Beijing
[2] State Key Laboratory of Chemical Safety, SINOPEC Research Institute of Safety Engineering Co., Ltd., Shandong, Qingdao
[3] State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing
来源
Huagong Xuebao/CIESC Journal | 2024年 / 75卷
关键词
detonation; hydrogen; instability; methane; multi-component; reaction kinetics;
D O I
10.11949/0438-1157.20240717
中图分类号
学科分类号
摘要
The detonation instability of two multi-component components with different C/H ratios is analyzed. Detonation experiments were carried out in a D=80 mm tube to analyze the characteristics of detonation velocity and cell structure changes of the multi-component components. The influence of hydrogen partial pressure on the instability of multi-component detonation was analyzed from the angle of three-wave point trajectory spacing, pitch and chemical reaction process. It is found that the detonation velocity of multi-component #1 is similar to that of hydrogen premixed gas, although it fluctuates, it is generally stable, and is always stable above 0.95VCJ. The detonation velocity of multi-component #2 is similar to that of methane premixed gas, and the fluctuation range is larger. From the perspective of cell structure characteristics, it is found that the variation trend of the number of detonation helical heads is similar to that of the velocity. The stability of component #1 is greater than that of component #2. The results are helpful to grasp the detonation propagation mechanism of multi-component. © 2024 Materials China. All rights reserved.
引用
收藏
页码:339 / 348
页数:9
相关论文
共 31 条
[1]  
Zhang K, Jin D, Song F L., Experimental research on nanosecond pulsed gliding arc discharge plasma cracking kerosene, Journal of Propulsion Technology, 43, 7, pp. 419-427, (2022)
[2]  
Liu M X, Tan N X, Wang J B., Mechanism construction and kinetic simulation for the combustion of cracked kerosene, Chem. Res. Appl, 31, pp. 278-282, (2019)
[3]  
Rudy W, Zbikowski M, Teodorczyk A., Detonations in hydrogen-methane-air mixtures in semi confined flat channels, Energy, 116, pp. 1479-1483, (2016)
[4]  
Bykovskii F A, Zhdan S A, Vedernikov E F., Continuous spin detonations, Journal of Propulsion and Power, 22, 6, pp. 1204-1216, (2006)
[5]  
Zhong Y P, Jin D, Wu Y, Et al., Investigation of rotating detonation wave fueled by “ethylene-acetylene-hydrogen” mixture, International Journal of Hydrogen Energy, 43, 31, pp. 14787-14797, (2018)
[6]  
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, Acta Astronautica, 157, pp. 310-320, (2019)
[7]  
Zhou S B, Ma H, Zhou C S, Et al., Experimental research on the propagation process of rotating detonation wave with a gaseous hydrocarbon mixture fuel, Acta Astronautica, 179, pp. 1-10, (2021)
[8]  
Han J X, Bai Q D, Qiu H, Et al., Influence of combustor configuration on rotating detonation characteristics of kerosene pre-combustion cracking gas, Acta Armrmamentarii, 45, 8, pp. 2837-2850, (2024)
[9]  
Chen H, Bai Q D, Weng C S., Research on cold flow mixing characteristics of kerosene pyrolysis gas in rotating detonation combustor, Journal of Ballistics, 35, 2, pp. 9-19, (2023)
[10]  
Wu M X, Bai Q D, Weng C S, Et al., Numerical simulation of rotating detonation wave propagation characteristics of C<sub>2</sub>H<sub>4</sub>/CH<sub>4</sub>/ H<sub>2</sub>mixture, Journal of Propulsion Technology, 43, 11, (2022)