Fatigue behavior of bonded composite repairs

Journal of Adhesion Science and Technology

Volumn 15, Issue 13, 2001, Pages 1621-1634

  Aglan, H ^a   Wang, Q Y ^a   Kehoe, M ^b  

^a TUSKEGEE UNIVERSITY   (United States)

^b NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

Author keywords

Aircraft structures; Bonded repair; Composite patches; Fatigue crack growth

Indexed keywords

ALUMINUM; BONDING; CRACK PROPAGATION; FATIGUE TESTING; MATHEMATICAL MODELS; STRESS INTENSITY FACTORS; SUBSTRATES; AIRCRAFT MANUFACTURE; AIRFRAMES; BORON; FATIGUE CRACK PROPAGATION; REPAIR;

COMPOSITE REPAIRS;

COMPOSITE MATERIALS; SUBSTRATES;

AIRCRAFT STRUCTURE; AL SUBSTRATE; ANALYTICAL MODEL; ANALYTICAL SOLUTIONS; BONDED COMPOSITE PATCH; BONDED COMPOSITE REPAIRS; BONDED REPAIRS; COMPOSITE PATCHES; COMPOSITE REPAIR; FATIGUE BEHAVIOR; FATIGUE TESTS; POWER LAW; RESEARCH AND DEVELOPMENT; TENSION-TENSION;

EID: 0035679336     PISSN: 01694243     EISSN: None     Source Type: Journal    
DOI: 10.1163/156856101753207715     Document Type: Article

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