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Numerical Simulation on Failure of Internally Pressured Cylinder Shell Under Laser irradiation

机译:内压缸壳激光辐照破坏的数值模拟

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The engine shell of the guide missile subjects to high-density internally pressure at normal active state. If it bears high-density laser irradiation, the temperature of the laser spot and adjacent materials will rise, localized thermal soft. The shell localized large deformation results in entirely bursting during thermal and mechanical acting. It is important academic and engineering worth to research failure of internally pressured cylinder shell under laser irradiation. To research the failure phenomenon, the thermal-mechanical coupling FEM is used in the paper. Heat conduction analysis coupled with strain rate is applied and factors such as the physical properties of material changing with the temperature are considered. The FEM results describe the whole phenomena, including thermal soften, large deformation and bursting of cylinder shell. And the time of shell failure with different internally pressure are obtained. The numerical results tally with those of Ref.
机译:在正常活动状态下,制导导弹的机壳承受高密度的内部压力。如果承受高密度激光照射,激光点和邻近材料的温度将升高,局部热软。壳体局部大变形导致在热作用和机械作用期间完全爆裂。研究内压气缸壳在激光辐照下的失效问题具有重要的学术和工程价值。为了研究故障现象,本文使用了热力耦合有限元法。结合应变率进行热传导分析,并考虑诸如材料的物理性质随温度变化的因素。有限元结果描述了整个现象,包括热软化,大变形和气缸壳破裂。并得到了不同内压下的壳破坏时间。数值结果与参考文献中的数值一致。

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