首页 | 本学科首页   官方微博 | 高级检索  
     检索      

炸药爆轰驱动超高速击波管的数值摸拟
引用本文:刘尔岩,袁仙春,廖振民.炸药爆轰驱动超高速击波管的数值摸拟[J].高压物理学报,1996,10(3).
作者姓名:刘尔岩  袁仙春  廖振民
作者单位:北京应用物理与计算数学研究所
基金项目:中国工程物理研究院科学基金
摘    要: 高能炸药(HE)柱壳沿轴向传播的稳定态爆轰,在置于炸药柱壳内部的泡沫塑料(工作流体)中产生很强的轴向击波,达到极高的压力和能量密度。适当设计,可使工作流体的流动接近一稳定态,与炸药爆轰以相同的相速度前进。击波阵面后的工作流体可用Nozzle流动方程很好地描述1],Nozzle收缩段中的流动不受散开段流动的影响。利用这一性质,可以设计出达到极高压力和能量密度的超高速击波管,并且不受管壁物质强度的限制。数值模拟计算给出了上述稳定态物理图象,并显示出开始阶段轴向击波的形成过程及其后对稳定态的逼近,计算结果及物理图象与理论分析符合得很好。

关 键 词:稳定态  相速度  Nozzle流
收稿时间:1995-12-22;

HYDRODYNAMICS CALCULATIONS OF THE FAST SHOCK TUBE DRIVED BY HIGH EXPLOSIVE
Liu Eryan,Yuan Xianchun,Liao Zhenmin.HYDRODYNAMICS CALCULATIONS OF THE FAST SHOCK TUBE DRIVED BY HIGH EXPLOSIVE[J].Chinese Journal of High Pressure Physics,1996,10(3).
Authors:Liu Eryan  Yuan Xianchun  Liao Zhenmin
Institution:Institute of Applied Physics and Computational Mathematics, Beijing 100088, China
Abstract:A phased implosion in a cylindrically high explosive(HE) shell can form extremely high pressures and energy densities in a low density foam core within shell. In a properly designed system, the flow of compressed foam approaches a steady state nozzle flow with the same velocity as that of detonation. The propagating wave decouples from the flow behind the sonic point. The flow can be used to produce shockless acceleration of masses to hypervelocities. The numerical simulations show the formation of the axial shock from the start to its approaching of its steady state, which is in good agreement with the theoretical analysis.
Keywords:phased  velocity    steady  state    nozzle  flow    
本文献已被 CNKI 等数据库收录!
点击此处可从《高压物理学报》浏览原始摘要信息
点击此处可从《高压物理学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号