Optimization of composite patch repair for center-cracked rectangular plate using design of experiments method

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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:	TL500 Aeronautics TS200 Metal manufactures. Metalworking
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

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