A study of the influence of drilling method and hole quality on static strength and fatigue life of carbon fiber reinforced plastic aircraft material

SAE Technical Papers

Volumn , Issue , 2002, Pages

  Johansson, Sten Å H ^a   Ossbahr, Gilbert C R ^a   Harris, Tom ^b  

^a LINKÖPING UNIVERSITY   (Sweden)

^b AIRBUS OPERATIONS LTD   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC EMISSION TESTING; AEROSPACE INDUSTRY; CARBON FIBER REINFORCED PLASTICS; CARBON FIBERS; FIBER REINFORCED PLASTICS; FRACTURE; FRACTURE MECHANICS; FRACTURE TESTING;

CARBON FIBRE COMPOSITE MATERIALS; COMPRESSION AND TENSION; DIFFERENT STAGES; DRILLING METHODS; FATIGUE PROPERTIES; FRACTURE BEHAVIOR; GEOMETRICAL PROPERTY; MEASUREMENT TECHNIQUES;

FATIGUE OF MATERIALS;

EID: 85072505966     PISSN: 01487191     EISSN: 26883627     Source Type: Journal    
DOI: 10.4271/2002-01-2650     Document Type: Conference Paper

References (3)

1. Persson, E., Machining and Fatigue Induced Damage in Bolted Composite Laminates, in Department of Aeronautics. 1998, Royal Institute of Technology: Stockholm.
2. Hart-Smith, L.J., Design and Analysis of Bolted and Riveted Joints in Fibrous Composite Structures. in International Symposium on Joining and Repair of Fibre-Reinforced Plastics. 1986. Imperial College London: HUCK.
3. König, W., and Grass P.,. Quality Definition and Assessment in Drilling of Fibre Reinforced Thermosets. in Annals of the CIRP. 1989. Trondheim: Hallwag Ltd.