Residual lifetime prediction in aerospace structures using wholefield laser strain techniques

Insight: Non-Destructive Testing and Condition Monitoring

Volumn 47, Issue 2, 2005, Pages 74-77

  Tyrer, John ^a   Petzing, Jon ^a   Ibrahim, Jamal ^a   Jones, Jones ^b   Lobo, Leon ^b  

^a LOUGHBOROUGH UNIVERSITY   (United Kingdom)

^b Laser Optical Engineering   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; COMPRESSION TESTING; DEFECTS; FRACTURE; IMAGE ANALYSIS; IMAGING SYSTEMS; LASER APPLICATIONS; PATTERN RECOGNITION; SENSORS; STRAIN; WHEELS;

AEROSPACE STRUCTURES; LASER SPECKLE STRAIN IMAGING; LASER STRAIN TECHNIQUES; LASER TECHNOLOGY; SPECKLE SHEARING INTERFEROMETRY; STRAIN MAPPER; WHOLEFIELD SENSOR SYSTEM;

NONDESTRUCTIVE EXAMINATION;

EID: 14044262871     PISSN: 13542575     EISSN: None     Source Type: Journal    
DOI: 10.1784/insi.47.2.74.58971     Document Type: Article

References (3)

1. Zhang, Z, Richardson, O, Tyrer, J R and Petzing, J N, 'Application of electronic speckle pattern interferometry to the testing of GRP composite materials', INSIGHT, 40(3), March 1998, pp 183-187, ISSN 1354-2575.
2. Tyrer, J R and Petzing, J N, 'In-plane electronic speckle pattern shearing interferometry', Journal of Optics & Lasers in Engineering 26(n4-5), 1997, pp 395-406, ISSN 0143-8166.
3. Wan Abdullah, W S, Petzing, J N and Tyrer, J R, 'Wave-Front Divergence: A Source of Error in Quantified Speckle Shearing Data', Journal of Modern Optics, 48(5), 2001, pp 757-772, ISSN 0950-0340.