偷看
材料科学
复合材料
本构方程
分离式霍普金森压力棒
应变率
热塑性复合材料
极限抗拉强度
航空航天
热塑性塑料
碳纤维增强聚合物
表征(材料科学)
结构工程
聚合物
有限元法
复合数
政治学
法学
工程类
纳米技术
作者
Aijia Li,Chunyang Chen,Chao Zhang,Yulong Li
出处
期刊:Earth and Space 2021
日期:2021-04-15
卷期号:30: 253-260
标识
DOI:10.1061/9780784483381.023
摘要
Thermoplastic composites have important applications in medical, electronics, automotive, and aerospace industries due to their good mechanical properties, easy for processing, recyclability, and low cost. In this work, the mechanical failure behavior of short carbon fiber reinforced PEEK composites is studied systemically using experimental technologies of quasi-static tests and dynamic Hopkinson bar tests. The experimental characterization covers different loading rate from 0.001 s to 1,000 s and temperature ranges from -30°C to 100°C, which provides detailed illustration for the effects of strain rate and temperature on the mechanical failure of short carbon fiber reinforced PEEK composites. The experimental results provide fundamental understandings on the failure mechanism of this material, especially in identifying the main factors affecting the rate-dependent and temperature-dependent behavior, which can facilitate the material design and model development. Based on the experimental data, this paper proposes an improved phenomenological constitutive model to describe the constitutive behavior of PEEK composites under different strain rates and different temperatures conditions.
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