Damage detection of the adhesive layer of Skin Doubler Specimens using SHM system based on fibre bragg gratings

Proceedings of the 5th European Workshop - Structural Health Monitoring 2010

Volumn , Issue , 2010, Pages 70-75

  Dvorak, M ^a   Ruzicka, M ^a   Kulisek, V ^a   Behal, J ^b   Kafka, V ^b  

^a CZECH TECHNICAL UNIVERSITY IN PRAGUE   (Czech Republic)

^b Aeronautical Research and Test Institute   (Czech Republic)

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVE LAYERS; ALUMINUM BODY; COATING MATERIAL; COMPOSITE PATCHES; DOUBLERS; FATIGUE CRACKING; FBG SENSOR; PATCH REPAIR;

ALUMINUM; DAMAGE DETECTION; FATIGUE TESTING; FIBER BRAGG GRATINGS; STRINGERS; STRUCTURAL HEALTH MONITORING;

ADHESIVES;

EID: 84861832479     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. th IWSHM, DEStech Publications, p. 167-174.
2. Baker, W., McKenzie, I., Jones, R. 2004. "Development of life extension strategies for Australian military aircraft, using structural health monitoring of composite repairs and joints," Composite Structures, 66: 133-143.
3. Baker, A., Rose, F., Jones, R. 2002. Advances in the Bonded Composite Repair of Metallic Aircraft Structure. Elsevier Science Ltd., Oxford.
4. Běhal, J. 2008. "Acoustic Emission Monitoring in the course of Strength Test of CFRP Aircraft Structure". Structural Health Monitoring, Krakow, ISBN 978-1-932078-94-7, p.1147-1151.