共 75 条
Experimental and numerical investigation on the premixed methane/air flame propagation in duct with obstacle gradients
被引:20
作者:
Zheng, Kai
[1
,4
,5
]
Jia, Qianhang
[1
]
Ma, Zimao
[2
]
Xing, Zhixiang
[1
]
Hao, Yongmei
[1
]
Yu, Minggao
[3
,6
]
机构:
[1] Changzhou Univ, Sch Safety Sci & Engn, Changzhou 213164, Peoples R China
[2] Chongqing Normal Univ, Coll Phys & Elect Engn, Chongqing 401331, Peoples R China
[3] Chongqing Univ, State Key Lab Coal Mine Disaster Dynam & Control, Chongqing 400044, Peoples R China
[4] State Key Lab Cultivat Base Gas Geol & Gas Control, Jiaozuo 454003, Henan, Peoples R China
[5] Gehu Rd, Changzhou, Jiangsu, Peoples R China
[6] 174 Shazhengjie, Chongqing 400030, Peoples R China
基金:
中国国家自然科学基金;
关键词:
Methane deflagration flame;
Obstacle gradient;
Flame speed;
Overpressure;
Numerical simulation;
TO-DETONATION TRANSITION;
HYDROGEN-AIR;
EXPLOSION CHARACTERISTICS;
BLOCKAGE RATIO;
TULIP FLAME;
ACCELERATION;
DEFLAGRATION;
CHANNEL;
OVERPRESSURE;
DYNAMICS;
D O I:
10.1016/j.psep.2023.08.077
中图分类号:
X [环境科学、安全科学];
学科分类号:
08 ;
0830 ;
摘要:
This work experimentally and numerically investigates the effect of the obstacle gradient on the characteristics of the methane/air explosion in obstructed ducts. The obstacle gradient is expressed through various blockage ratios, and three different obstacle gradients are investigated, i.e., C357, C555, and C753. Noted that C357 means that the blockage ratios of three obstacles arranged sequentially in the duct are 0.3, 0.5 and 0.7 respectively, and so do C555 and C753. A two-dimensional (2D) model is adopted and the Scale-Adaptive Simulation method with the thickened flame model is considered. Experimental results show that the obstacle gradient significantly affects the flame evolution structure, flame propagation speed and overpressure. The obstacle gradient is accountable for the "tulip flames" appearing downstream of the obstacle. For the case with a fixed methane volume fraction, the average flame front speed is fixed. However, with the increasing obstacle gradient, the maximum flame front speed increases until it achieves the maximum at C357, and so does the maximum overpressure. The numerical simulation can predict the flame evolution behaviour precisely. It is evident that the generation of different flame shapes appearing is derived from the flow field evolution of unburned gas downstream of the flame front.
引用
收藏
页码:893 / 904
页数:12
相关论文