Experimental study on fatigue resistance of composite joints with protruding-head bolts

Composite Structures

Volumn 55, Issue 1, 2002, Pages 1-11

  Starikov, Roman ^a   Schön, Joakim ^b  

^a ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

^b Aeronautical Research Institute of Sweden   (Sweden)

Author keywords

Composite joints; Fatigue durability; Load transfer; Strain

Indexed keywords

BOLTS; CARBON FIBERS; DILATOMETERS; FATIGUE TESTING; STRAIN GAGES;

FATIGUE RESISTANCE;

JOINTS (STRUCTURAL COMPONENTS);

COMPOSITE; FATIGUE; STRAIN;

EID: 0036138626     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(01)00127-1     Document Type: Article

References (15)

1. Certification of damage tolerant composite structures
2. Common failure modes for composite aircraft structures due to secondary loads
3. Damage tolerance and durability testing for F/A-18 E/F composite materials structures
4. Strength and lifetime of bolted laminates
5. Effect of environment and improvement measures on static and fatigue strength of bolted CFRP-joints
6. Fatigue failure of bolted joints
7. Fatigue of multiple-row bolted joints in carbon/epoxy laminates: Ranking of factors affecting strength and fatigue life
8. Quasi-static behaviour of composite joints with protruding-head bolts
9. Spectrum fatigue of composite bolted joints
10. Coefficient of friction of composite delamination surfaces
11. Fatigue resistance of composite joints with countersunk composite and metal fasteners
12. Failure mechanism in compression-loaded composite laminates containing open and filled holes
13. Analysis methods for bolted composite joints subjected to in-plane shear loads
14. Decay of end effects in graphite/ epoxy bolted joints