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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| פורמט: | Thesis |
| שפה: | English |
| יצא לאור: |
2015
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| גישה מקוונת: | http://psasir.upm.edu.my/id/eprint/65496/1/FK%202015%20149IR.pdf |