Durability assessment of composite repairs bonded to aircraft structures

Journal of Adhesion Science and Technology

Volumn 13, Issue 1, 1999, Pages 127-148

  Aglan, H ^a   Rowell, T ^a   Ahmed, T ^b   Thomas, R ^b  

^a TUSKEGEE UNIVERSITY   (United States)

^b WAYNE STATE UNIVERSITY   (United States)

Author keywords

Aircraft structures: composite repairs; Delamination; Durability

Indexed keywords

ALUMINUM; BORON; CRACK PROPAGATION; DELAMINATION; DURABILITY; EPOXY RESINS; FATIGUE TESTING; HYSTERESIS; INFRARED IMAGING; REPAIR; TENSILE TESTING; THERMAL CYCLING; AIRCRAFT MANUFACTURE; AIRFRAMES; CRACKS; RIVETS; ROCK DRILLS;

THERMAL WAVE IMAGING;

AIRCRAFT MATERIALS; SUBSTRATES;

AIRCRAFT SKIN; AIRCRAFT STRUCTURE; ALUMINUM SUBSTRATE; COMPOSITE REPAIR; CRACK ARREST; DISBOND; DOUBLERS; DURABILITY ASSESSMENT; FATIGUE LIFETIME; FATIGUE LOADINGS; LONG TERM PERFORMANCE; MECHANICAL FATIGUE; MECHANICAL TENSION; MULTI-SITE; RESIDUAL STRENGTH; RIVET HOLE; TENSILE LOADING; THERMAL CYCLE; THERMAL WAVE IMAGING;

EID: 0032794941     PISSN: 01694243     EISSN: 15685616     Source Type: Journal    
DOI: 10.1163/156856199X00343     Document Type: Article

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