Review of nondestructive testing methods for fiber⁃reinforced polymer composites

被引：0
作者：
Huang L. [1 ]
机构：
[1] School of Aeronautics, Northwestern Polytechnical University, Xi’an
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2024年 / 45卷 / 05期
关键词：
Analytic Hierarchy Process (AHP); damage detection; fibre-reinforced polymer composites; hybrid non-destructive testing techniques; non-destructive testing;
D O I：
10.7527/S1000-6893.2023.29697
中图分类号：
学科分类号：
摘要：
In recent years，Fiber-Reinforced Polymer（FRP）composites have seen a significant increase in their application scope due to their exceptional mechanical properties and remarkable weight advantages. However，due to their intricate damage modes，it is crucial to employ advanced damage characterization methods to mitigate potential catastrophic consequences. Currently，a wide range of Non-Destructive Testing and Evaluation（NDT&E）techniques have been extensively employed in the damage detection of FRP composite. These techniques have undergone continuous development and enhancement，enabling reliable structural examination，particularly in the aerospace industry. This article will initially provide a comprehensive overview of the latest advancements in non-destructive testing techniques within the FRP composite material damage diagnosis，providing intensive analysis and evaluation of ten NDT technologies，namely acoustic emission test，ultrasonic test，Infrared thermography test，shearography test，digital image correlation test，eddy current test，terahertz imaging test，microwave test，electrical tomography imaging test and X-ray test，assessing the advantages and limitations of each technique. Subsequently，based on specific criteria，these non-destructive testing techniques will be assessed. However，as single non-destructive testing techniques struggle to achieve unified functions such as defect identification，localization，classification，and evaluation，a combination of non-destructive testing is proposed as a solution to achieve enhanced outcomes in practical engineering applications. © 2024 Chinese Society of Astronautics. All rights reserved.
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