Fatigue life modeling of FRP composites: A comprehensive review

被引:10
|
作者
Ganesan, C. [1 ]
Joanna, P. S. [2 ]
Singh, Dalbir [1 ]
机构
[1] Hindustan Inst Technol & Sci, Sch Aeronaut Sci, Chennai 603103, Tamil Nadu, India
[2] Hindustan Inst Technol & Sci, Dept Civil Engn, Chennai 603103, Tamil Nadu, India
关键词
Fatigue life; Damage; GFRP; CFRP; Residual Strength; Stiffness; RESIDUAL STRENGTH DEGRADATION; CONSTANT-AMPLITUDE; FABRIC COMPOSITES; PREDICTION; BEHAVIOR; FAILURE; RATIOS;
D O I
10.1016/j.matpr.2020.11.119
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Advanced composites have been widely used in various industries ranging from aerospace to medical equipment due to its exceptional characteristics under different circumstances. Fatigue behavior of composite structures and in particular fatigue life modeling is an important area of research in the context of aircraft structures since the behavior of composite material is different from monolithic metals. This article focusses on the review of modeling the fatigue life and residual strength of different composite materials under various loading conditions. Models based on residual strength, stiffness and damage tolerance techniques are reviewed and discussed. (c) 2021 Elsevier Ltd. All rights reserved. Selection and peer-review under responsibility of the scientific committee of the 2nd International Conference on Manufacturing Material Science and Engineering.
引用
收藏
页码:555 / 561
页数:7
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