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Damage mechanism of gamma-irradiated repurposed pultruded glass fibre polyester composite subjected to low-velocity impact using non-destructive techniques

Muhammad Imran Najeeb Muhammad Amir Siti Madiha Agusril Syamsir Mohd Supian Abu Bakar Sapizah Rahim Asyraf Arif Abu Bakar Tabrej Khan

防务技术2025，Vol.47Issue(5)：139-151,13.

防务技术2025，Vol.47Issue(5)：139-151,13.DOI:10.1016/j.dt.2025.01.002

Damage mechanism of gamma-irradiated repurposed pultruded glass fibre polyester composite subjected to low-velocity impact using non-destructive techniques

Muhammad Imran Najeeb ¹Muhammad Amir Siti Madiha ²Agusril Syamsir ³Mohd Supian Abu Bakar ⁴Sapizah Rahim ²Asyraf Arif Abu Bakar ²Tabrej Khan⁵

作者信息

1. Department of Engineering Education,Faculty of Engineering and Built Environment,Universiti Kebangsaan Malaysia,Bangi,43600,Malaysia
2. Industrial Technology Division,Malaysian Nuclear Agency,Bangi,Kajang,43000,Malaysia
3. Institute of Energy Infrastructure,Universiti Tenaga Nasional,Jalan IKRAM-UNITEN,Kajang,43000,Malaysia||Civil Engineering Department,College of Engineering,Universiti Tenaga Nasional,Jalan IKRAM-UNITEN,Kajang,43000,Malaysia
4. Institute of Energy Infrastructure,Universiti Tenaga Nasional,Jalan IKRAM-UNITEN,Kajang,43000,Malaysia
5. Department of Engineering Management,College of Engineering,Prince Sultan University,Riyadh,11586,Saudi Arabia
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摘要

关键词

Damage mechanism/Low-velocity impact/Gamma irradiation/Non-destructive methods/Composite failure analysis/Energy

Key words

Damage mechanism/Low-velocity impact/Gamma irradiation/Non-destructive methods/Composite failure analysis/Energy

引用本文复制引用

Muhammad Imran Najeeb,Muhammad Amir Siti Madiha,Agusril Syamsir,Mohd Supian Abu Bakar,Sapizah Rahim,Asyraf Arif Abu Bakar,Tabrej Khan..Damage mechanism of gamma-irradiated repurposed pultruded glass fibre polyester composite subjected to low-velocity impact using non-destructive techniques[J].防务技术,2025,47(5):139-151,13.

基金项目

This research was funded by Universiti Tenaga Nasional(UNI-TEN),Malaysia for supporting this research under the Dato' Low Tuck Kwong International Grant,project code 20238002DLTK.The authors would like to acknowledge the support for this work from the Ministry of Higher EducationMalaysia through the Higher Institution Center of Excellence(HICoE 2023-JPT(BPKI)1000/016/018/34(5))program.This work was also supported by Tenaga Nasional Berhad(TNB)and UNITEN through the BOLD Refresh Postdoctoral Fellowships under Grant J510050002-IC-6 BOLDRE-FRESH2023-Centre of Excellence.The author would like to thank Prince Sultan University for their support.The authors would like to thank Industrial Technology Division,Malaysian Nuclear Agency for their support in this research work. （UNI-TEN）

防务技术

ISSN：2214-9147

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