High-velocity impact and post-impact fatigue response of Bismaleimide resin composite laminates

IF 4.4 2区 工程技术 Q1 MECHANICS
Zhenhua Zhao , Fengrui Liu , Xin Yang , Zhihao Xie , Lulu Liu , Wei Chen
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引用次数: 0

Abstract

Bismaleimide (BMI) resin composite is a kind of thermoplastic composite that has attracted a lot of attention for its advantages in fracture toughness and damage tolerance. The composite structures are usually exposed to the threat of foreign object impact during service; static strength and fatigue resistance of composite structures with impact damage will dramatically degrade, which can lead to catastrophic damage of composite structures. In this paper, the hard foreign objects and air cannon were used to conduct a high-speed impact test on the BMI composite laminate. The effect of impactor diameter, impact velocity, and impact angle on impact damage size and microscopic damage mechanism was investigated; respectively, the results show that damage width and length increase with the growth of impact velocity and impactor size, the impact velocity has a greater impact on damage depth, and various impact angles will significantly change the damage morphology. After impact, the step-by-step method was used to analyze the fatigue strength of composite laminates with impact damage; it was found the depth of impact damage has the biggest impact on the fatigue strength. Based on conclusions of the fatigue test, a prediction model was proposed to predict the fatigue strength of composite laminate with the impact damages; the results show that prediction results are within 1.5 times of the error band. This paper reveals the damage behavior of composite laminate under high-speed impact; the proposed fatigue strength prediction method can provide a reference for the safety evaluation of composite structures.
双马来酰亚胺树脂复合层压板的高速冲击及冲击后疲劳响应
双马来酰亚胺(BMI)树脂复合材料是一种热塑性复合材料,因其在断裂韧性和损伤容限方面的优势而备受关注。复合材料结构在使用过程中经常受到外来物冲击的威胁;复合材料结构发生冲击损伤后,其静力强度和抗疲劳性能会急剧下降,从而导致复合材料结构的灾难性损伤。本文采用硬异物和空气炮对BMI复合材料层压板进行了高速冲击试验。研究了冲击器直径、冲击速度和冲击角度对冲击损伤尺寸和微观损伤机理的影响;结果表明:损伤宽度和长度随冲击速度和冲击器尺寸的增大而增大,冲击速度对损伤深度的影响较大,不同的冲击角度会显著改变损伤形态;冲击后,采用分步法对复合材料层合板进行了疲劳强度分析;结果表明,冲击损伤深度对疲劳强度的影响最大。根据疲劳试验的结论,提出了考虑冲击损伤的复合材料层合板疲劳强度预测模型;结果表明,预测结果在误差带的1.5倍以内。揭示了复合材料层合板在高速冲击下的损伤行为;提出的疲劳强度预测方法可为复合材料结构的安全性评价提供参考。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
7.00
自引率
7.30%
发文量
275
审稿时长
48 days
期刊介绍: The European Journal of Mechanics endash; A/Solids continues to publish articles in English in all areas of Solid Mechanics from the physical and mathematical basis to materials engineering, technological applications and methods of modern computational mechanics, both pure and applied research.
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