Numericalsimulationofair/steeltargetinterface effectsonparallelinjectingshapedchargejet
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摘要: 利用非线性动力学软件LS-DYNA,对聚能射流平行入射大气/钢靶板交界处的侵彻过程进行了数 值模拟。通过分析数值模拟过程和结果,讨论了聚能射流头部速度和碰撞出口处横向速度的变化规律。结果 表明:大气/钢靶板交界处不仅降低了聚能射流头部的轴向速度,而且使射流头部产生横向偏移,最大速度达 到约1.8km/s;后续射流横向偏移速度逐渐减小,导致聚能射流提前断裂,未能形成连续侵彻。因此,大气/ 钢靶板交界处对聚能射流的头部起到了明显的干扰作用,可有效降低射流的侵彻能力。Abstract: BasedonthenonlineardynamicssoftwareLS-DYNA,thecompleteprocessofjetparallel penetratingair/steeltargetinterfacewasnumericallysimulated.Byanalyzingtheprocessandresultof numericalsimulation,thevelocityoftheshapedchargejettipandthetransversevelocityafterimpact werediscussed.Theresultsshowthatattheair/steeltargetinterfacetheaxialvelocityoftheshaped chargejettipdecreasesevidentlyandtheshapedchargejettipisreducedtomovingtransversely,the highesttransversevelocityofwhichisabout1.8km/s;thatthetransversevelocitiesofthesubsequentjetsdecreasegraduallyandthejetdisruptionisantedated. Consequently,theair/steeltargetinterfacecanmarkedlydisturbtheshapedchargejettipandeffectivelyweakenthejetpenetration.
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Key words:
- mechanicsofexplosion /
- shapedcharge /
- LS-DYNA /
- disruption /
- penetration /
- transverse velocity
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