薄层复合材料冲击损伤行为研究进展
曹勇1,2, 张超3,4,5
1. 太原理工大学 机械与运载工程学院 应用力学研究所, 太原 030024;
2. 材料强度与结构冲击山西省重点实验室, 太原 030024;
3. 西北工业大学 航空学院, 西安 710072;
4. 西北工业大学 民航学院, 太仓 215400;
5. 陕西省冲击动力学及工程应用重点实验室, 西安 710072
CAO Yong1,2, ZHANG Chao3,4,5
1. Institute of Applied Mechanics, College of Mechanical and Vehicle Engineering, Taiyuan University of Technology, Taiyuan 030024, China;
2. Shanxi Key Laboratory of Material Strength & Structural Impact, Taiyuan 030024, China;
3. School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China;
4. School of Civil Aviation, Northwestern Polytechnical University, Taicang 215400, China;
5. Shaanxi Key Laboratory of Impact Dynamics and Its Engineering Applications, Xi'an 710072, China
摘要: 采用展宽减薄丝束的薄层复合材料具有显著的就位效应,导致其变形和失效机制更为复杂,并显现出不同于常规的损伤失效规律,引起了科研工作者的广泛关注。本文从薄层复合材料冲击损伤角度回顾了自薄层复合材料工业化应用以来,各类薄层复合材料冲击失效模式、层间断裂韧性和计算分析方法的研究现状,总结分析了降低单层厚度对复合材料冲击损伤行为的影响规律以及薄层复合材料冲击仿真分析的建模要点,展望了薄层复合材料冲击损伤研究待解决的关键科学问题和未来的研究要点。
关键词: 薄层复合材料, 展宽减薄工艺, 冲击损伤, 断裂韧性, 有限元分析
Abstract: Thin-ply composites show more obvious in-situ effect, which results in more complicated deformation and failure mechanisms, as well as variations in damage and failure behaviors. Focused on the impact behavior of thin-ply composites, this paper reviews the research advances on the impact failure mechanism, intralaminar fracture behavior and computational modeling methods of thin-ply composites. The effect of ply thickness on the impact damage behavior of thin-ply composites and the critical points for impact simulation are summarized and discussed. The key problems and major research directions for future studies in impact failure analysis of thin-ply composites are also discussed.
Key words: thin-ply composite, spread-tow thin-ply technology, impact damage, damage tolerance, finite element analysis
引用本文