玻-碳混杂纤维缠绕复合材料发射筒发射动力学研究

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Abstract In order to simulate the motion process of projectile in bore accuracy, the two-dimensional transient distribution characteristics of the propellant gas pressure in a glass/carbon hybrid filament winding composite launch canister was considered.Based on the contact collision theory and considering the strong dynamic impact of propellant gas, a numerical analysis model for the nonlinear coupling problems between the projectile and the launch canister was built.A user-defined subroutine was used to reconstruct the correlation kinetic process between the temporal and spatial variation of propellant gas pressure and the projectile motion.Numerical analysis results were compared with test data.The results show that the established numerical analysis model can reproduce the physical field changes in the actual launching process and the dynamics stress response of launch canister can be simulated more actually, providing a theoretical support for the design, optimization ,and launch safety evaluation of the fiber composite launch canister.

Key words： glass/carbon hybrid launch canister user-defined subroutine projectile-barrel coupling finite element analysis

Received: 10 July 2018 Published: 15 December 2019

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	Articles by authors
	SUN Tongsheng1
	WANG Qi2
	YU Cungui1

Cite this article:

SUN Tongsheng1,WANG Qi2,YU Cungui1. A study on firing dynamics of a glass/carbon hybrid filament winding composite launch canister[J]. JOURNAL OF VIBRATION AND SHOCK, 2019, 38(24): 74-80.

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http://jvs.sjtu.edu.cn/EN/ OR http://jvs.sjtu.edu.cn/EN/Y2019/V38/I24/74

[1] 徐光磊, 杨庆平, 阮文俊,等. 考虑混杂效应时纤维混杂缠绕筒三维等效弹性模量的理论估算和试验研究[J]. 复合材料学报, 2012, 29(4):204-209.
XU Guang-lei, YANG Qing-ping, RUAN Wen-jun. Estimation and experiment of 3D effective elastic modulus for fiber hybrid tube considering hybrid effects [J]. Acta material composite sinica, 2012, 29(4):204-209.
[2] 徐光磊, 阮文俊, 王浩,等. 含内衬纤维缠绕筒水压试验分析[J]. 兵器材料科学与工程, 2012, 35(4):27-29.
XU Guang-lei, RUAN Wen-jun, WANG Hao, et al. Hydrostatic test for fiber filament-wound tube with lining [J]. Ordnance material science and engineering, 2012, 35(4):27-29.
[3] 尹冬梅, 栗保明. 考虑缠绕预应力的轨道炮身管复合外壳渐进损伤分析[J]. 兵工学报, 2016, 37(6):988-995.
YIN Dong-mei, LI Bao-ming. Analysis of progressive damage of composite housing for railgun under winding prestress [J]. Acta armamentarii, 2016, 37(6):988-995.
[4] Lehmann P, Vo M D, Wenning W. Comparative study of railgun housings made of modern fiber wound materials, ceramic, or insulated steel plates[J]. IEEE Transactions on Magnetics, 2005, 41(1):200-205.
[5] 朱孙科, 马大为, 罗天洪,等. 基于有限元动力学的复合材料发射筒多目标优化设计[J]. 机械科学与技术, 2012, 31(6):74-78.
ZHU Sun-ke, MA Da-wei, LUO Tian-hong, et al. Multi-objective optimization of composite launch canister based on finite element dynamics[J]. Mechanical science and technology for aerospace engineering, 2012, 31(6):74-78.
[6] 朱孙科, 马大为, 于存贵,等. 多管火箭炮定向管的多目标优化及多属性决策研究[J]. 兵工学报, 2010, 31(11):1413-1417.
ZHU Sun-ke, MA Da-wei, YU Cun-gui, et al. Study on MRLS direction pipe’s multi-objective optimization and multi-attribute decision making[J]. Acta armamentarii, 2010, 31(11):1413-1417.
[7] 宋云雪, 史永胜, 王晓鸣. 复合材料火箭发射管有限元分析[J]. 南京理工大学学报(自然科学版), 2000, 24(5):418-420.
SONG Yun-xue, SHI Yong-sheng, WANG Xiao-ming. The finite element analysis for the composite rocket launching case[J]. Journal of Nanjing university of science and technology, 2000, 24(5):418-420.
[8] 王轲, 张福祥. 玻璃钢制火箭炮定向器的强度研究[J]. 弹道学报, 2003, 15(2):39-43.
WANG Ke, ZHANG Fu-xiang. The strength research of the rocket launcher GFRP tube[J]. Journal of ballistics, 2003, 15(2):39-43.
[9] Tzeng J T. Dynamic response and fracture of composite cylinders[J]. Composites Science & Technology, 1998, 58(9):1443-1451.
[10]Tzeng J T. Structural mechanics for electromagnetic railguns[J]. IEEE Transactions on Magnetics, 2005, 41(1):246-250.
[11]杨宇宙. 复合材料身管的损伤研究[D]. 南京理工大学, 2013.
YANG Yu-zhou. Study on damage of the composite barrel[D]. Nanjing university of science and technology, 2013.
[12]徐亚栋. 复合材料身管动态响应分析[D]. 南京理工大学, 2003.
XU Ya-dong. Analysis of dynamic response for composite barrel[D]. Nanjing university of science and technology, 2003.
[13]魏存磊, 徐亚栋, 马燕颖. 瞬态冲击载荷下复合材料身管损伤研究[J]. 兵器装备工程学报, 2016, 37(7):131-136.
WEI Cun-lei, XU Ya-dong, MA Yan-ying. Study on damage of composite material barrel under transient impact load[J]. Journal of ordnance equipment engineering, 2016, 37(7):131-136.
[14]葛建立, 杨国来, 陈运生,等. 基于弹塑性接触/碰撞模型的弹炮耦合问题研究[J]. 弹道学报, 2008, 20(3):103-106.
GE Jian-li, YANG Guo-lai, CHEN Yun-sheng, et al. A study on projectile-barrel coupling problem based on elastoplastic contact/impact model[J]. Journal of ballistics, 2008, 20(3):103-106.
[15]刘书, 刘晶波, 方鄂华. 动接触问题及其数值模拟的研究进展[J]. 工程力学, 1999, 16(6):14-28.
LIU Shu, LIU Jing-bo, FANG E Hua. The advances of studies on the dynamic contact problem and its numerical methods[J]. Engineering mechanics, 1999, 16(6):14-28.
[16]B Nour-Omid, P Wriggers. A two-level iteration method for solution of contact problems[J]. Computer Methods in Applied Mechanics & Engineering, 1986, 54:131-144.
[17]Zhang XB, Wang YZ. Analysis of dynamic characteristics for rarefaction wave gun during the launching[J]. Journal of Applied Mechanics. 2010 Sep 1; 77(5):051601.
[18]苏忠亭, 徐达, 李晓伟,等. 小口径火炮弹炮耦合动态响应有限元时程分析[J]. 振动与冲击, 2012, 31(23):104-108.
SU Zhong-ting, XU Da, LI Xiao-wei,et al. Finite-element time-history analysis for dynamic response of small-caliber guns with projectile-barrel coupling[J]. Journal of Vibration And Shock, 2012,31(23):104-108.
[19]李小珍,张志俊,刘全民. 任意移动荷载列作用下简支梁桥竖向振动响应解析分析[J]. 振动与冲击, 2012,31(20): 137-142.
LI Xiao-zhen, ZHANG Zhi-jun, LIU Quan-min. Vertical dynamic response analysis of a simply supported beam bridge under successive moving loads[J]. Journal of vibration and shock, 2012,31(20): 137-142.