首页> 外文会议>The 2nd joint US-Canada conference on composites, American Society for Composites 26th annual technical conference. >Computational Simulation and Experimental Characterization of Sandwich Composite Panels Subjected to Blast Loads
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Computational Simulation and Experimental Characterization of Sandwich Composite Panels Subjected to Blast Loads

机译:爆炸荷载作用下夹芯复合板的计算模拟与实验表征

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Blast response experimental data along with quasi-static material property datarnwas generated for E-glass and carbon sandwich composite panels with balsa, PVCrnfoam and TYCOR? cores. In this work the Pressure vs Impulse (P-I) curvernmethodology that was developed to represent estimated damage levels in civilrninfrastructure components subjected to blast loadings, is adapted for sandwichrncomposite panels. This enables the generation of a database of performancernenvelopes of sandwich composite panels with a variety of skin and core materialrncombinations under various blast and shock loading scenarios, for naval compositernstructural applications. The P-I diagram (also known as iso-damage curve)rnmathematically relates a specific damage level to a combination of blast pressurernand impulse imposed on a particular structural element, allowing the reduced orderrnmodeling of different composite panel system configurations. Each curve in the P-Irndiagram represents a certain response level, such as mid-span deflection or rotationrnat supports.rnThe strength vs deformation properties of various undamaged sandwichrncomposite panels are established by nonlinear quasi-static finite element analysis ofrnsandwich composite panels subjected to mid-span deformation under displacementrncontrol, with boundary conditions matching that of the experimental blast tests andrnidealized for SDOF (single degree of freedom) modeling. Nonlinear stress-strainrnmaterial data obtained from quasi-static tensile tests of face sheets and compressiverntesting of corresponding core materials is used as input for the material constitutivernmodels. Numerical simulations of reduced order, i.e. equivalent SDOF systemrnmodels of the blast loaded sandwich composite panels are conducted; to enable thernconstruction of iso-damage curves that are suitable for damage prediction over arnwider range of blast pressure and impulse combinations. Results show goodrncorrespondence between model predictions and experimental results for thernperformance evaluation of various sandwich composite panel configurations.
机译:生成了具有轻木,PVC泡沫和TYCOR的E玻璃和碳夹芯复合板的爆炸响应实验数据以及准静态材料性能数据。核心。在这项工作中,开发了压力-冲击(P-I)曲线方法,以表示承受爆炸载荷的民用基础设施组件的估计破坏水平,该方法适用于夹芯复合板。这使得能够生成在各种爆炸和冲击载荷情况下具有多种表皮和核心材料组合的夹芯复合材料面板性能信封的数据库,用于海军复合结构应用。 P-I图(也称为等损伤曲线)在数学上将特定的损伤程度与施加在特定结构元件上的爆炸压力和冲击力的组合相关联,从而可以简化不同复合板系统配置的阶次建模。 P型图表中的每条曲线代表一定的响应水平,例如中跨挠度或旋转支承。通过对中夹层复合板进行非线性准静态有限元分析,可以确定各种未损坏的夹芯复合板的强度与变形特性。位移控制下的跨度变形,边界条件与爆炸试验的边界条件相匹配,并且对SDOF(单自由度)建模进行了理想化。从面板的准静态拉伸测试和相应核心材料的压缩测试获得的非线性应力应变材料数据用作材料本构模型的输入。进行了降阶的数值模拟,即爆炸加载的夹芯复合板的等效SDOF系统模型;以便能够构建适合在爆炸压力和冲击组合的更广范围内进行损伤预测的等损伤曲线。结果表明,模型预测值与实验结果之间具有良好的对应关系,可用于评估各种夹芯复合板结构的性能。

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