Optimization of composite patch repair for center-cracked rectangular plate using design of experiments method
The repair of aircraft structures using composite material patches are well known in aerospace industries. In the present work composite patch bonded with a superglue over a cracked rectangular plate under uniform uniaxial tensile stress is considered. A three-dimensional finite element method was u...
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| Main Authors: | , , |
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| Format: | Proceeding Paper |
| Language: | en en en |
| Published: |
Elsevier Ltd
2020
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/81790/13/81790_Optimization%20of%20composite%20patch%20repair%20for%20center-cracked.pdf http://irep.iium.edu.my/81790/7/81790_Optimization%20of%20composite%20patch%20repair%20for%20center-cracked_SCOPUS.pdf http://irep.iium.edu.my/81790/14/81790_Optimization%20of%20composite%20patch%20repair%20for%20center-cracked_WOS.pdf http://irep.iium.edu.my/81790/ https://www.sciencedirect.com/science/article/pii/S2214785320324214 |
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