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Numerical Simulating and Experimental Study on the Woven Carbon Fiber-Reinforced Composite Laminates under Low-Velocity Impact

机译:低速冲击下纺织碳纤维增强复合层压层的数值模拟与实验研究

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Impact damage has been identified as a critical form of the defects that constantly threatened the reliability of composite structures, such as those used in the aerospace structures and systems. Low energy impacts can introduce barely visible damage and cause the degradation of structural stiffness, furthermore, the flaws caused by low-velocity impact are so dangerous that they can give rise to the further extended delaminations. In order to improve the reliability and load carrying capacity of composite laminates under low-velocity impact, in this paper, the numerical simulatings and experimental studies on the woven fiber-reinforced composite laminates under low-velocity impact with impact energy 16.7J were discussed. The low velocity impact experiment was carried out through drop-weight system as the reason of inertia effect. A numerical progressive damage model was provided, in which the damages of fiber, matrix and interlamina were considered by VUMT subroutine in ABAQUS, to determine the damage modes. The Hashin failure criteria were improved to cover the failure modes of fiber failure in the directions of warp/weft and delaminations. The results of Finite Element Analysis (FEA) were compared with the experimental results of nondestructive examination including the results of ultrasonic C-scan, cross-section stereomicroscope and contact force - time history curves. It is found that the response of laminates under low-velocity impact could be divided into stages with different damage. Before the max-deformation of the laminates occurring, the matrix cracking, fiber breakage and delaminations were simulated during the impactor dropping. During the releasing and rebounding period, matrix cracking and delaminations areas kept increasing in the laminates because of the stress releasing of laminates. Finally, the simulating results showed the good agreements with the results of experiment.
机译:影响损坏已被确定为缺陷的临界形式,这些缺陷不断威胁复合结构的可靠性,例如航空航天结构和系统中使用的那些。低能量撞击可以引入几乎可见的损坏并导致结构刚度的降低,此外,低速撞击引起的缺陷是如此危险,它们可以产生进一步的扩展分层。为了提高较低速度冲击下复合层压板的可靠性和承载能力,本文讨论了对薄丝纤维增强复合层压材料的数值模拟和实验研究,其低速冲击与冲击能量16.7J。低速冲击实验是通过滴重系统作为惯性效应的原因进行的。提供了一种数值渐进式损伤模型,其中通过ABAQUS中的VUMT子程序考虑了纤维,基质和层间损伤,以确定损坏模式。哈希林故障标准得到改善,以覆盖经线/纬纱和分层方向上的纤维失效模式。将有限元分析(FEA)的结果与非破坏性检查的实验结果进行了比较,包括超声C扫描,横截面立体显微镜和接触力 - 时历史曲线的结果。发现层压板在低速冲击下的响应可以分为不同损伤的阶段。在发生层压材料的最大变形之前,在撞击过程中模拟了基质裂化,纤维破裂和分层。在释放和反弹期间,由于层压板的应力释放,基质裂缝和分层区域在层压板中保持增加。最后,模拟结果表明了与实验结果的良好协议。

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