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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Bibliographic Details
Main Authors: Aabid, Abdul, Hrairi, Meftah, Mohamed Ali, Jaffar Syed
Format: Proceeding Paper
Language:English
English
English
Published: Elsevier Ltd 2020
Subjects:
Online Access:http://irep.iium.edu.my/81790/
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