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Response of S2-Glass/Vinyl Ester Composites under High Strain Rate Loading - An Experimental and Finite Element Study

机译:S2-玻璃/乙烯基酯复合材料在高应变速率下的响应-实验和有限元研究

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Thick-section S2-Glass/Vinyl Ester composites are used as a structural component in the construction of integral armor. The external ceramic layer of the integral armor acts as a ballistic shield, and the thick composite layer of the interior takes the structural loads as well as it serves as a backing plate for the armor. While the integral armor in its entirety is being treated in another paper, this paper deals with the response of the composite layer alone. Split Hopkinson Pressure Bar (SHPB) has been used extensively to determine the strength of the composite both in the thickness and fiber directions. The strain rate sensitivity of the material has also been determined, and the failure modes are identified. Transient dynamic Finite Element Analysis (FEA) has been performed up to maximum strain rate of 1700 s~(-1). Two different loading conditions similar to experiments are used; one in the thickness direction and the other in the fill direction of the composite specimen. Layered 3D solid elements have been used to model the composite specimens. Transient dynamic analysis has been carried out with incremental time steps, and the stiffness matrix has been considered as a function of displacement and time. Time dependent loading similar to experiments in SHPB is applied as distributed force on the loading surface. Stress propagation and its distribution through the thickness of the laminate are presented. It is observed that FEA can only predict the initial state of deformation of the specimen because the stress computations are based on linear elasticity. It is also revealed from the FEA that during fill direction loading, both interlaminar tensile and shear stresses occur simultaneously at the very initial stage of the loading and cause the specimens to delaminate at a lower stress. The failure modes during the thickness direction loading are however, different. Detailed description of the experimental observations and FEM modeling are presented in this paper.
机译:厚截面的S2-玻璃/乙烯基酯复合材料用作整体装甲的结构部件。整体装甲的外部陶瓷层充当防弹盾,内部的厚复合层承担结构载荷,并充当装甲的背板。虽然在另一篇文章中讨论了整体装甲,但本文仅涉及复合层的响应。斯普利特霍普金森压力棒(SHPB)已被广泛用于确定复合材料在厚度和纤维方向上的强度。还确定了材料的应变率敏感性,并确定了失效模式。最高动态应变速率为1700 s〜(-1),已进行了瞬态动态有限元分析(FEA)。使用类似于实验的两种不同的加载条件;一个在厚度方向上,另一个在填充样品的填充方向上。分层3D实体元素已用于对复合材料样本进行建模。瞬态动力学分析已按递增的时间步长进行,刚度矩阵已被视为位移和时间的函数。类似于SHPB中实验的随时间变化的载荷作为分布力施加在载荷面上。给出了应力传播及其在层压板厚度上的分布。可以观察到,FEA只能预测样品变形的初始状态,因为应力计算基于线性弹性。从有限元分析中还可以看出,在填充方向加载期间,层间拉伸应力和剪切应力在加载的最开始阶段同时发生,并导致样品在较低应力下分层。然而,在厚度方向加载期间的失效模式是不同的。本文介绍了实验观察结果和有限元模型的详细描述。

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