Performance and Modeling of a Two-Stage Light Gas Gun Driven by Gaseous Detonation

被引:10
作者
Tang, Weiqi [1 ,2 ]
Wang, Qiu [3 ]
Wei, Bingchen [1 ,2 ,4 ]
Li, Jiwei [3 ]
Li, Jinping [3 ]
Shang, Jiahao [2 ,3 ]
Zhang, Kun [1 ]
Zhao, Wei [2 ,3 ]
机构
[1] Chinese Acad Sci, Inst Mech, Key Lab Micrograv, Natl Micrograv Lab, Beijing 100190, Peoples R China
[2] Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China
[3] Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
[4] Univ Chinese Acad Sci, Ctr Mat Sci & Optoelect Engn, Beijing 100049, Peoples R China
来源
APPLIED SCIENCES-BASEL | 2020年 / 10卷 / 12期
基金
中国国家自然科学基金;
关键词
two-stage light gas gun; detonation; quasi-one-dimensional; piston; projectile; RANGE;
D O I
10.3390/app10124383
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
A two-stage light gas gun driven by gaseous detonation was newly constructed, which can make up for the disadvantages of the insufficient driving capability of high-pressure gas and the constraints of gunpowder. The performance of the gas gun was investigated through experiments and a quasi-one-dimensional modeling of it was also developed and described in detail. The model accounts for the friction and heat transfer to the tube wall for gases by adding a source term. An improved model has been established to consider the inertial loads in the piston or projectile and model the friction force with the tube wall. Besides, the effects of pump tube pressure on the performance of the gas gun are also investigated numerically. Simulations of the pressure histories in the pump tube and the piston and projectile velocities were conducted. A good agreement was observed between the computational predictions and experimental results. The results showed that the friction between the piston and wall had only small influence on the piston velocity. The proposed numerical approach is suitable for the development of two-stage light gas guns and tests of the operating conditions.
引用
收藏
页数:16
相关论文
共 30 条
[1]  
Batchelor P.L., 2010, THESIS
[2]  
Bird G.A., 1957, NOTE COMBUSTION DRIV, V146
[3]  
Bogdanoff DW, 1995, NEW HIGHER ORDER GOD
[4]  
Canning T.N., 1970, Ballistic - Range Technology
[5]   Large-scale, hypervelocity, high-fidelity interceptor lethality development in AEDC's range G [J].
Carver, D. ;
Campbell, L. L. ;
Roebuck, B. .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2008, 35 (12) :1459-1464
[6]  
Chapman G., 1992, P 17 AER GROUD TEST, P3996
[7]  
Charters A. C., 1987, Int. J. Impact Eng., V5, P181, DOI DOI 10.1016/0734-743X(87)90038-8
[8]   Driver gas contaminationin a detonation-driven reflected-shock tunnel [J].
Chue, RSM ;
Tsai, CY ;
Bakos, RJ .
SHOCK WAVES, 2004, 13 (05) :367-380
[9]   HIGH-VELOCITY, LIGHT-GAS GUN [J].
CROZIER, WD ;
HUME, W .
JOURNAL OF APPLIED PHYSICS, 1957, 28 (08) :892-894
[10]  
[邓飞 Deng Fei], 2014, [兵工学报, Acta Armamentarii], V35, P415