Quasi-static strength and fatigue life of hybrid (bonded/bolted) composite single-lap joints

Composite Structures

Volumn 72, Issue 1, 2006, Pages 119-129

  Kelly, Gordon ^a  

^a ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

Author keywords

Composite; Fatigue life; Finite element analysis; Hybrid (bonded bolted); Single lap joint; Strength

Indexed keywords

ADHESION; BOND STRENGTH (MATERIALS); CARBON FIBER REINFORCED PLASTICS; COMPOSITE STRUCTURES; CRACK INITIATION; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; STIFFNESS; STRENGTH OF MATERIALS;

FAILURE MODE; FATIGUE CRACK INITIATION; HYBRID COMPOSITE; SINGLE-LAP JOINT;

JOINTS (STRUCTURAL COMPONENTS);

CARBON FIBER; FIBER REINFORCED COMPOSITE; LIFE PREDICTION; STRENGTH;

EID: 28644435669     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2004.11.002     Document Type: Article

References (15)

1. L.J. Hart-Smith Bonded-bolted composite joints J Aircraft 22 11 1985 993-1000
2. Hart-Smith LJ. Design methodology for bonded-bolted composite joints. Technical Report AFWAL-TR-81-3154, Douglas Aircraft Company; 1982.
3. W.S. Chan S. Vedhagiri Analysis of composite bolted/bonded joints used in repairing J Compos Mater 35 12 2001 1045-1061
4. Montabone M, Nebiolo M, Vigada C. An investigation on a bolted-cold bonded joint for large diameter structures. In: 83rd Meeting of the AGARD SMP on bolted/bonded joints in polymeric composites, CP 590, Florence, Italy; 1996.
5. Fu Maofeng P.K. Mallick Fatigue of hybrid (adhesive/bolted) joints in SRIM Int J Adhes Adhes 21 2001 145-159
6. M. Imanaka K. Haraga T. Nishikawa Fatigue strength of adhesive/rivet combined lap joints J Adhesion 49 1995 197-209
7. G. Kelly Load transfer in hybrid (bolted/bonded) composite single-lap joints J Compos Struct 69 1 2005 35-43
8. Z. Zhang J.K. Shang F.V. Lawrence A backface strain technique for detecting fatigue crack initiation in adhesive joints J Adhesion 49 1995 23-36
9. ASTM D 638 02a Standard test method for tensile properties of plastics. American Society for Testing and Materials; 2002.
10. G. Kelly S. Hallström Bearing strength of carbon fibre epoxy laminates: Effects of bolt hole clearance Composites Part B 35 4 2004 331-343
11. A. Crocombe C.Y. Ong C.M. Chan M.M. Abdel Wahab I.A. Ashcroft Investigating fatigue damage evolution in adhesive bonded structures using backface strain measurement J Adhesion 78 2002 745-776
12. Hibbet, Karlsson, and Sorensen Inc. Abaqus/standard user's manuals, V6.4. Pawtucket, RI, USA; 2003.
13. DiNicola AJ, Fantle SL. Bearing strength of clearance fit fastener holes in toughened grTphite/epoxy laminates. In: Composite materials: testing and design, vol. 11. ASTM STP 1206; 1993. p. 220-37.
14. M.A. McCarthy V.P. Lawlor W.F. Stanley C.T. McCarthy Bolt-hole clearance effects and strength criteria in single-bolt, single-lap, composite bolted joints Compos Sci Technol 62 10-11 2002 1415-1431
15. Truong Chi T, Lomov SV, Verpoest I. The mechanical properties of multi-axial multi-ply carbon fabric reinforced epoxy composites. In Proceedings of the 10th European conference on composite materials (ECCM-10), Brugge, Belgium; 2002.