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A combined experimental and numerical approach to study ballistic impact response of S2-glass fiber/toughened epoxy composite beams

机译:结合实验和数值方法研究S2-玻璃纤维/增韧环氧复合材料梁的弹道冲击响应

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摘要

A combined experimental and 3D dynamic nonlinear finite element (FE) approach was adopted to study damage in composite beams subject to ballistic impact using a high-speed gas gun. The time-histories of dynamic strains induced during impact were recorded using strain gages mounted on the front of the composite beam specimen. During ballistic impact tests, the impact velocity was also measured. The commercially available 3D dynamic nonlinear FE code, LS-DYNA, modified with a proposed user-defined nonlinear-orthotropic damage model, was then used to simulate the experimental results. In addition, LS-DYNA with the Chang-Chang linear-orthotropic damage model was also used for comparison. Good agreement between experimental and FE results was found from the comparisons of dynamic strain and damage patterns. Once the proposed nonlinear-orthotropic damage model was verified by experimental results, further FE simulations were conducted to predict the ballistic limit velocity (V_(50)) using either the number of damaged layer approach or a numerically established relation between the projectile impact velocity versus residual velocity or energy similar to the classical Lambert-Jonas equation for metals.
机译:结合实验和3D动态非线性有限元(FE)方法,研究了使用高速气枪在弹道冲击下对复合梁的损伤。使用安装在复合梁样品前部的应变计记录了在冲击过程中引起的动态应变的时程。在弹道冲击试验中,还测量了冲击速度。然后使用经提议的用户定义的非线性正交各向异性损伤模型修改的市售3D动态非线性FE代码LS-DYNA来模拟实验结果。此外,还使用具有常场线性正交各向异性损伤模型的LS-DYNA进行比较。通过动态应变和损伤模式的比较发现实验结果和有限元结果之间有很好的一致性。一旦通过实验结果验证了所提出的非线性正交各向异性损伤模型,便会进行进一步的有限元仿真,以使用损伤层数方法或弹丸撞击速度与弹丸速度之间的数值关系来预测弹道极限速度(V_(50))。残余速度或能量类似于金属的经典Lambert-Jonas方程。

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