兵器材料科学与工程
兵器材料科學與工程
병기재료과학여공정
Ordnance Material Science and Engineering
2013年
3期
83-85
,共3页
臧立伟%尹建平%王志军%王潞红
臧立偉%尹建平%王誌軍%王潞紅
장립위%윤건평%왕지군%왕로홍
爆炸力学%爆炸成型弹丸(EFP)%尾翼%数值模拟
爆炸力學%爆炸成型彈汍(EFP)%尾翼%數值模擬
폭작역학%폭작성형탄환(EFP)%미익%수치모의
explosive mechanics%explosively formed projectile(EFP)%fin%numerical simulation
利用LS-DYNA显示动力分析有限元程序,采用流固耦合方法,对带尾翼EFP的形成过程进行数值模拟。结果表明:该装药结构能形成带有8个尾翼的EFP,带尾翼EFP的长径比是EFP长径比的2.23倍,其头部速度比EFP增加了15%。
利用LS-DYNA顯示動力分析有限元程序,採用流固耦閤方法,對帶尾翼EFP的形成過程進行數值模擬。結果錶明:該裝藥結構能形成帶有8箇尾翼的EFP,帶尾翼EFP的長徑比是EFP長徑比的2.23倍,其頭部速度比EFP增加瞭15%。
이용LS-DYNA현시동력분석유한원정서,채용류고우합방법,대대미익EFP적형성과정진행수치모의。결과표명:해장약결구능형성대유8개미익적EFP,대미익EFP적장경비시EFP장경비적2.23배,기두부속도비EFP증가료15%。
Numerical simulation of the forming process of the fin?adhered EFP was carried out with the ALE method using LS?DYNA. The result indicates that such a charge structure can form EFP with eight fins,the length?diameter ratio of EFP with fins is 2.23 times than that of EFP without fins,and velocity increases by 15 percent.