Characterization of Degradation Progressive in Composite Laminates Subjected to Thermal Fatigue and Moisture Diffusion by Lamb Waves

Laminate composites which are widely used in the aeronautical industry, are usually subjected to frequency variation of environmental temperature and excessive humidity in the in-service environment. The thermal fatigue and moisture absorption in composites may induce material degradation. There is...

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Main Authors: Weibin Li, Chunguang Xu, Younho Cho
Format: Article
Language:English
Published: MDPI AG 2016-02-01
Series:Sensors
Subjects:
Online Access:http://www.mdpi.com/1424-8220/16/2/260
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spelling doaj-5da577fbd8214a06b4edb777c1df655b2020-11-24T23:18:56ZengMDPI AGSensors1424-82202016-02-0116226010.3390/s16020260s16020260Characterization of Degradation Progressive in Composite Laminates Subjected to Thermal Fatigue and Moisture Diffusion by Lamb WavesWeibin Li0Chunguang Xu1Younho Cho2School of Aerospace Engineering, Xiamen University, Xiamen 361005, ChinaSchool of Mechanical Engineering, Beijing Institute of Technology, Beijing 100041, ChinaSchool of Mechanical Engineering, Pusan National University, Busan 609-735, KoreaLaminate composites which are widely used in the aeronautical industry, are usually subjected to frequency variation of environmental temperature and excessive humidity in the in-service environment. The thermal fatigue and moisture absorption in composites may induce material degradation. There is a demand to investigate the coupling damages mechanism and characterize the degradation evolution of composite laminates for the particular application. In this paper, the degradation evolution in unidirectional carbon/epoxy composite laminates subjected to thermal fatigue and moisture absorption is characterized by Lamb waves. The decrease rate of Lamb wave velocity is used to track the degradation evolution in the specimens. The results show that there are two stages for the progressive degradation of composites under the coupling effect of thermal cyclic loading and moisture diffusion. The present work provides an alternative to monitoring the degradation evolution of in-service aircraft composite Laminates.http://www.mdpi.com/1424-8220/16/2/260composite laminatesdegradation progressivethermal fatiguemoisture diffusionLamb waves
collection DOAJ
language English
format Article
sources DOAJ
author Weibin Li
Chunguang Xu
Younho Cho
spellingShingle Weibin Li
Chunguang Xu
Younho Cho
Characterization of Degradation Progressive in Composite Laminates Subjected to Thermal Fatigue and Moisture Diffusion by Lamb Waves
Sensors
composite laminates
degradation progressive
thermal fatigue
moisture diffusion
Lamb waves
author_facet Weibin Li
Chunguang Xu
Younho Cho
author_sort Weibin Li
title Characterization of Degradation Progressive in Composite Laminates Subjected to Thermal Fatigue and Moisture Diffusion by Lamb Waves
title_short Characterization of Degradation Progressive in Composite Laminates Subjected to Thermal Fatigue and Moisture Diffusion by Lamb Waves
title_full Characterization of Degradation Progressive in Composite Laminates Subjected to Thermal Fatigue and Moisture Diffusion by Lamb Waves
title_fullStr Characterization of Degradation Progressive in Composite Laminates Subjected to Thermal Fatigue and Moisture Diffusion by Lamb Waves
title_full_unstemmed Characterization of Degradation Progressive in Composite Laminates Subjected to Thermal Fatigue and Moisture Diffusion by Lamb Waves
title_sort characterization of degradation progressive in composite laminates subjected to thermal fatigue and moisture diffusion by lamb waves
publisher MDPI AG
series Sensors
issn 1424-8220
publishDate 2016-02-01
description Laminate composites which are widely used in the aeronautical industry, are usually subjected to frequency variation of environmental temperature and excessive humidity in the in-service environment. The thermal fatigue and moisture absorption in composites may induce material degradation. There is a demand to investigate the coupling damages mechanism and characterize the degradation evolution of composite laminates for the particular application. In this paper, the degradation evolution in unidirectional carbon/epoxy composite laminates subjected to thermal fatigue and moisture absorption is characterized by Lamb waves. The decrease rate of Lamb wave velocity is used to track the degradation evolution in the specimens. The results show that there are two stages for the progressive degradation of composites under the coupling effect of thermal cyclic loading and moisture diffusion. The present work provides an alternative to monitoring the degradation evolution of in-service aircraft composite Laminates.
topic composite laminates
degradation progressive
thermal fatigue
moisture diffusion
Lamb waves
url http://www.mdpi.com/1424-8220/16/2/260
work_keys_str_mv AT weibinli characterizationofdegradationprogressiveincompositelaminatessubjectedtothermalfatigueandmoisturediffusionbylambwaves
AT chunguangxu characterizationofdegradationprogressiveincompositelaminatessubjectedtothermalfatigueandmoisturediffusionbylambwaves
AT younhocho characterizationofdegradationprogressiveincompositelaminatessubjectedtothermalfatigueandmoisturediffusionbylambwaves
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