A Structural Health Monitoring (SHM) of composite patch repair for aircraft part and structures using principal component analysis

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A Structural Health Monitoring (SHM) of composite patch repair for aircraft part and structures using principal component analysis

The use of advanced composite structures on aircraft is increasing. New aircraft, such as the Airbus A350 and the Boeing B787, have more than 50% of their structure originating from composite materials especially carbon fiber reinforced plastic (CFRP). Delamination, disbonding, voids and barely visi...

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Bibliographic Details
Main Author:	Mohd Aris, Khairul Dahri
Format:	Thesis
Language:	English
Published:	2015
Subjects:	Structural health monitoring - Automation Airplanes - Parts
Online Access:	http://psasir.upm.edu.my/id/eprint/65496/ http://psasir.upm.edu.my/id/eprint/65496/1/FK%202015%20149IR.pdf

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