基于DIC分析的三维角互锁编织凯夫拉/环氧复合材料低速冲击损伤实验评估

IF 2.9 4区 材料科学 Q3 MATERIALS SCIENCE, COMPOSITES
Xinyu Tian, Huajun Ding, Bohong Gu
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引用次数: 0

摘要

本文研究了三维编织凯夫拉/环氧复合材料在动态冲击条件下的损伤和能量吸收,以阐明其抗冲击性能。低速冲击试验采用落锤试验机,在不同的速度下进行。结合载荷-位移曲线和能量吸收结果,结合损伤形态分析,确定了不同的损伤模式和完全侵彻的临界能量。采用高速成像技术结合数字图像相关(DIC)技术对冲击过程中的全场应变分布和损伤演化进行了研究。实现了一种增强的损伤跟踪算法,该算法专门针对大的面外变形和不连续设计,可以广泛适用于其他材料系统的大面外变形。结果表明,最大载荷随冲击速度的增加而增加,而弯曲刚度保持不变。在较低的速度(1m /s)下,观察到具有明显反弹的弹性行为,没有分层或穿透。在2 m/s时,确定穿透能阈值为44.3 J,而在3 m/s时,复合材料完全穿透,最大载荷、位移和塑性能吸收均有所增加。冲击速度越高,裂纹越长,由于纬纱的直线排列,纬纱裂纹的长度始终超过经纱裂纹,有利于损伤的扩展。显微组织分析表明,纤维断裂、界面脱落和基体开裂是三维编织凯夫拉/环氧复合材料的主要破坏模式。这些发现为三维编织复合材料的损伤机制、应变演化和力学行为提供了有价值的见解。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental Assessment of Low Velocity Impact Damage in 3D Angle-Interlock Woven Kevlar/Epoxy Composite Using DIC Analysis

This study investigates the damage and energy absorption of 3D woven Kevlar/epoxy composites under dynamic impact conditions to clarify their impact resistance. Low velocity impact tests were conducted using a drop weight tester at various velocities. Load-displacement curves and energy absorption results, combined with damage morphology analysis, were used to identify different damage modes and the critical energy for complete penetration. High-speed imaging combined with digital image correlation (DIC) technique was employed to examine the full-field strain distribution and damage evolution during the impact process. An enhanced damage-tracking algorithm was implemented, specifically designed for large out-of-plane deformations and discontinuities and could be broadly applicable to other material systems that undergo large out-of-plane deformations. Results showed that maximum load increased with impact velocity, while bending stiffness remained constant. At lower velocities (1 m/s), elastic behavior with significant rebound was observed, with no delamination or penetration. At 2 m/s, the penetration energy threshold was determined to be 44.3 J, while at 3 m/s, the composite was fully penetrated, showing increased maximum load, displacement, and plastic energy absorption. Higher impact velocities led to longer cracks, with weft cracks consistently exceeding warp cracks in length due to the straight arrangement of weft yarns, which facilitates damage propagation. Microstructural analysis identified fiber fracture, interfacial debonding, and matrix cracking as the main failure modes of the 3D woven Kevlar/epoxy composite. These findings provide valuable insights into the damage mechanisms, strain evolution, and mechanical behavior of 3D woven composites.

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来源期刊
Applied Composite Materials
Applied Composite Materials 工程技术-材料科学:复合
CiteScore
4.20
自引率
4.30%
发文量
81
审稿时长
1.6 months
期刊介绍: Applied Composite Materials is an international journal dedicated to the publication of original full-length papers, review articles and short communications of the highest quality that advance the development and application of engineering composite materials. Its articles identify problems that limit the performance and reliability of the composite material and composite part; and propose solutions that lead to innovation in design and the successful exploitation and commercialization of composite materials across the widest spectrum of engineering uses. The main focus is on the quantitative descriptions of material systems and processing routes. Coverage includes management of time-dependent changes in microscopic and macroscopic structure and its exploitation from the material''s conception through to its eventual obsolescence.
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