Analysis of aircraft adhesive joints under combined thermal and mechanical cyclic loadings

Journal of Adhesion Science and Technology

Volumn 11, Issue 7, 1997, Pages 941-956

  Abdo, Z ^a   Aglan, H ^a  

^a TUSKEGEE UNIVERSITY   (United States)

Author keywords

Aircraft adhesive joints; Fatigue disbond propagation; Specific energy of damage; Thermal aging

Indexed keywords

AGING OF MATERIALS; AIRCRAFT PARTS AND EQUIPMENT; CRACK PROPAGATION; DEFORMATION; ENERGY DISSIPATION; FATIGUE OF MATERIALS; FRACTURE TOUGHNESS; THERMAL CYCLING; THERMAL EFFECTS; THERMAL LOAD; ADHESIVE JOINTS; AIRCRAFT; FATIGUE CRACK PROPAGATION; LOADING; TESTING;

FATIGUE DISBOND PROPAGATION; MECHANICAL CYCLING; SPECIFIC ENERGY OF DAMAGE;

ADHESIVE JOINTS; THERMAL AGING;

AGING CYCLE; AIR CONDITIONS; ALUMINUM 7075-T6; CYCLIC LOADINGS; DAMAGE CONCEPT; ENERGY DISSIPATION COEFFICIENT; FATIGUE BEHAVIOR; FATIGUE LOADINGS; JOINT RESISTANCE; LOAD CARRYING CAPACITIES; LOAD-DISPLACEMENT CURVE; LOW TEMPERATURES; PREPREGS; SINGLE LAP JOINTS; SPECIFIC ENERGY; STATIC DEFORMATIONS; STATIC LOADING; STRUCTURAL ADHESIVE; TEST PROCEDURES; THERMAL AND MECHANICAL CYCLING;

EID: 0030658434     PISSN: 01694243     EISSN: 15685616     Source Type: Journal    
DOI: 10.1163/156856197X00516     Document Type: Article

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