Strain rate effect on mode I debonding characterization of adhesively bonded aluminum joints

In adhesive bonding, two different substrate materials are joined together, usually by forming chemical bonds. The adhesive can stick things together. The loading rate and deformation mode can easily change the mechanical properties of the adhesive material. Hence, a vital aim of the current study i...

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التفاصيل البيبلوغرافية
المؤلفون الرئيسيون: Khan, Safdar Ali, Koloor, Seyed Saeid Rahimian, Wong, King Jye, Yidris, Noorfaizal, Mohd. Yusof, Ab. Aziz, Mohd. Szali Januddi, Mohd. Al Fatihhi, Tamin, Mohd. Nasir, Johar, Mahzan
التنسيق: مقال
اللغة:English
منشور في: MDPI 2023
الموضوعات:
الوصول للمادة أونلاين:http://eprints.utm.my/106534/1/WongKingJye2023_StrainRateEffectonModeIDebonding.pdf
http://eprints.utm.my/106534/
http://dx.doi.org/10.3390/pr11010081
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spelling my.utm.1065342024-07-09T06:46:37Z http://eprints.utm.my/106534/ Strain rate effect on mode I debonding characterization of adhesively bonded aluminum joints Khan, Safdar Ali Koloor, Seyed Saeid Rahimian Wong, King Jye Yidris, Noorfaizal Mohd. Yusof, Ab. Aziz Mohd. Szali Januddi, Mohd. Al Fatihhi Tamin, Mohd. Nasir Johar, Mahzan TJ Mechanical engineering and machinery In adhesive bonding, two different substrate materials are joined together, usually by forming chemical bonds. The adhesive can stick things together. The loading rate and deformation mode can easily change the mechanical properties of the adhesive material. Hence, a vital aim of the current study is to evaluate the strain rate effect on the damage response of adhesive joints for Mode I loading scenarios. The adherend material was aluminum AL6061-T6, and Araldite 2015 was the adherent material. This experiment for delamination had a prescribed adherend size of 200 mm × 25 mm × 3 mm and an adhesive thickness of 0.5 mm. In situations where the strain rate affects the failure mechanism, a displacement rate of 5, 50, or 500 mm/min is sufficient to attain the failure mechanism. A double cantilever beam (DCB) specimen was employed to construct the FE model geometry for simulation. A hybrid experimental–FE technique was utilized to extract the properties of the adhesive interface. FE simulation has proven to have an excellent correlation with the experimental findings. MDPI 2023-01 Article PeerReviewed application/pdf en http://eprints.utm.my/106534/1/WongKingJye2023_StrainRateEffectonModeIDebonding.pdf Khan, Safdar Ali and Koloor, Seyed Saeid Rahimian and Wong, King Jye and Yidris, Noorfaizal and Mohd. Yusof, Ab. Aziz and Mohd. Szali Januddi, Mohd. Al Fatihhi and Tamin, Mohd. Nasir and Johar, Mahzan (2023) Strain rate effect on mode I debonding characterization of adhesively bonded aluminum joints. Processes, 11 (1). pp. 1-14. ISSN 2227-9717 http://dx.doi.org/10.3390/pr11010081 DOI:10.3390/pr11010081
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
language English
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Khan, Safdar Ali
Koloor, Seyed Saeid Rahimian
Wong, King Jye
Yidris, Noorfaizal
Mohd. Yusof, Ab. Aziz
Mohd. Szali Januddi, Mohd. Al Fatihhi
Tamin, Mohd. Nasir
Johar, Mahzan
Strain rate effect on mode I debonding characterization of adhesively bonded aluminum joints
description In adhesive bonding, two different substrate materials are joined together, usually by forming chemical bonds. The adhesive can stick things together. The loading rate and deformation mode can easily change the mechanical properties of the adhesive material. Hence, a vital aim of the current study is to evaluate the strain rate effect on the damage response of adhesive joints for Mode I loading scenarios. The adherend material was aluminum AL6061-T6, and Araldite 2015 was the adherent material. This experiment for delamination had a prescribed adherend size of 200 mm × 25 mm × 3 mm and an adhesive thickness of 0.5 mm. In situations where the strain rate affects the failure mechanism, a displacement rate of 5, 50, or 500 mm/min is sufficient to attain the failure mechanism. A double cantilever beam (DCB) specimen was employed to construct the FE model geometry for simulation. A hybrid experimental–FE technique was utilized to extract the properties of the adhesive interface. FE simulation has proven to have an excellent correlation with the experimental findings.
format Article
author Khan, Safdar Ali
Koloor, Seyed Saeid Rahimian
Wong, King Jye
Yidris, Noorfaizal
Mohd. Yusof, Ab. Aziz
Mohd. Szali Januddi, Mohd. Al Fatihhi
Tamin, Mohd. Nasir
Johar, Mahzan
author_facet Khan, Safdar Ali
Koloor, Seyed Saeid Rahimian
Wong, King Jye
Yidris, Noorfaizal
Mohd. Yusof, Ab. Aziz
Mohd. Szali Januddi, Mohd. Al Fatihhi
Tamin, Mohd. Nasir
Johar, Mahzan
author_sort Khan, Safdar Ali
title Strain rate effect on mode I debonding characterization of adhesively bonded aluminum joints
title_short Strain rate effect on mode I debonding characterization of adhesively bonded aluminum joints
title_full Strain rate effect on mode I debonding characterization of adhesively bonded aluminum joints
title_fullStr Strain rate effect on mode I debonding characterization of adhesively bonded aluminum joints
title_full_unstemmed Strain rate effect on mode I debonding characterization of adhesively bonded aluminum joints
title_sort strain rate effect on mode i debonding characterization of adhesively bonded aluminum joints
publisher MDPI
publishDate 2023
url http://eprints.utm.my/106534/1/WongKingJye2023_StrainRateEffectonModeIDebonding.pdf
http://eprints.utm.my/106534/
http://dx.doi.org/10.3390/pr11010081
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