In-situ health monitoring of a bonded composite patch using the strain ratio technique

Proceedings of SPIE- The International Society for Optical Engineering

Volumn 4235, Issue , 2001, Pages 363-374

  Moss, S D ^a   Galea, S C ^a   Powlesland, I G ^a   Konak, M ^a   Baker, A A ^a  

^a AERO AND MAR RESEARCH LABORATORY   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVES; ALGORITHMS; CYCLIC LOADS; FATIGUE TESTING; PIEZOELECTRIC DEVICES; SENSORS; STRAIN MEASUREMENT;

PIEZO-ELECTRIC (PVDF) SENSORS; SMART PATCH DEVICES;

COMPOSITE STRUCTURES;

EID: 0034988448     PISSN: 0277786X     EISSN: None     Source Type: Journal    
DOI: 10.1117/12.420878     Document Type: Article

References (9)

1. Crack patching: "Experimental studies, practical applications"
2. Repair of cracked or defective metallic aircraft components with advanced fibre composites- An overview of Australian work
3. Bonded composite repair of metallic aircraft components
4. Repair substantiation for a bonded composite repair to a F-111 lower wing skin
5. On the certification of bonded composite repairs to primary aircraft structures
6. A smart patch approach for bonded composite repairs to primary airframe structures
7. Fatigue testing of bonded joints representative of the F111C WPF upper plate doublers