期刊文献+

约束空间内爆超压载荷影响因素二维数值模拟 被引量:1

Two-dimensional numerical simulation of the factors influencing the explosion overpressure load inside the confined space
下载PDF
导出
摘要 [目的]为了研究炸药运动、初始界面扰动及网格尺寸对舱内爆炸超压载荷的影响规律,[方法]采用五阶WNEO有限差分格式、三阶TVD龙格—库塔法对二维可压缩欧拉方程的空间项和时间项进行数值离散,并基于Fortran平台,自主开发约束空间内爆炸波高精度数值计算程序,利用所开发的程序对舱内爆炸超压载荷的影响因素进行初步探讨。[结果]研究表明,增大炸药运动速度、选取特定的初始界面扰动、减小网格尺寸均能较明显地提高舱内爆炸冲击波峰值,但对准静态超压载荷的影响较小。[结论]研究结果可为抗爆结构设计及舱内爆炸毁伤评估提供一定的参考和指导。 [Objectives]In order to study how dynamic motion of explosive,initial interface disturbance and grid size affect the overpressure load of internal explosion,[Methods]the spatial and temporal terms of the two-dimensional compressible Euler equations are discretized numerically using the fifth-order WNEO finite difference scheme and the third-order TVD Runge-Kutta scheme.Based on Fortran platform,an in-house high-precision numerical calculation program of blast wave in confined space was developed.The impacts of the overpressure load of the internal explosion were preliminarily discussed adopting the developed program.[Results]The results show that,increasing charge movement speed,selecting a specific interface disturbance and decreasing the size of the grid can significantly increase shock wave peaks of internal explosion,but has little effect on quasi-static overpressure load.[Conclusions]The research in this paper can provide certain reference and basis for the design of anti-explosion structure and the evaluation of internal explosion damage.
作者 徐维铮 吴卫国 Xu Weizheng;Wu Weiguo(Key Laboratory of High Performance Ship Technology of Ministry of Education,Wuhan University of Technology,Wuhan 430063,China;School of Transportation,Wuhan University of Technology,Wuhan 430063,China)
出处 《中国舰船研究》 CSCD 北大核心 2019年第2期91-98,共8页 Chinese Journal of Ship Research
基金 国家自然科学基金资助项目(51409202) 装备预研教育部联合基金青年人才项目资助(6141A02331) 中央高校基本科研业务费专项资金资助项目(2016-YB-016)
关键词 约束空间 爆炸冲击载荷 超压载荷 炸药运动 界面扰动 网格尺寸 数值计算 confined space impulsive load overpressure load explosive movement interface perturbation grid size numerical simulation
  • 相关文献

参考文献8

二级参考文献23

  • 1丁阳,陈晔,师燕超.室内爆炸超压荷载简化模型[J].工程力学,2015,32(3):119-125. 被引量:13
  • 2侯海量,朱锡,梅志远.舱内爆炸载荷及舱室板架结构的失效模式分析[J].爆炸与冲击,2007,27(2):151-158. 被引量:75
  • 3孙承纬,卫玉章,周之奎.理论爆轰物理[M].北京:国防工业出版社,2000:130-138.
  • 4Chang S C.The method of space-time conservation element and solution element-A new approach for solving the Navier-Stokes equations[J].Journal of Computational Physics,1995,191:295-324.
  • 5Wang X Y,Chow C Y,Chang S C.Application of the space-time conservation element and solution element method to shock-tube problem[R].NASA TM-1068086,1994:1-35.
  • 6ZHANG Zeng-chan,HE Hao,Chang S C,et al.Direct calculations of two-and three-dimensional detonations by an extended CE/SE method[R].AIAA 2001-0476,2001:1-5.
  • 7SENG T I,YANG R J.Simulation of the Mach reflection in supersonic flows by the CE/SE method[J].Shock Waves,2005,14(4):307-311.
  • 8CHING Y L,ZAMAN K B M Q.Numerical investigation of 'transonic resonance' with a convergent-divergent nozzle[R].AIAA 2002-0077,2002:1-13.
  • 9CHANG S C,YU S T.Robust and simple non-reflecting boundary conditions for the Euler equationsA new approach based on the Space-Time CE/SE Method[J].NASA/TM-2003-212495,2003:1-40.
  • 10杨亚政,李松年,杨嘉陵.高超音速飞行器及其关键技术简论[J].力学进展,2007,37(4):537-550. 被引量:43

共引文献58

同被引文献9

引证文献1

二级引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部