Load transfer in multirow, single shear, composite-to-aluminium lap joints
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Abstract
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Research context
OpenAlex topics: Structural Load-Bearing Analysis · Structural Behavior of Reinforced Concrete · Mechanical Behavior of Composites
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References (27)
Show source-provided references
1. Observations on bolted connections in composite structures
2. Delamination onset prediction in mechanically fastened joints in composite laminates10.1177/002199839903301002 ↗
3. Strength of mechanically fastened composite joints10.1177/002199838201600603 ↗
4. Bearing strength behavior of clearance-fit fastener holes in toughened graphite/epoxy laminates
5. E.T. Camponeschi, Jr., (Ed.), ASTM STP 1206, American Society for Testing and Materials, Philadelphia.
6. Secondary bending in multi fastener, composite-to-aluminium single shear lap joints10.1016/j.compositesb.2004.09.001 ↗
7. P. Ericsson, Bestämning av sekundärböjning och lastöverföringsfördelningar hos enskärigt bultförband. Technical report, The Aeronautical Research Institute of Sweden, 1983. FFA TN 1983-17 [in Swedish].
8. Design of multiple-row bolted composite joints under general in-plane loading10.1016/0961-9526(95)00044-N ↗
9. Strength prediction of mechanically fastened quasi-isotropic carbon/epoxy joints10.1177/002199839603001405 ↗
10. Hart-Smith LJ. Bolted joints in graphite-epoxy composites. Technical Report NASA CR-144899, Douglas Aircraft Company, June 1976.
11. Hart-Smith LJ. The design of efficient bolted and riveted fibrous composite structures. Technical Report Douglas Paper 8335, Douglas Aircraft Company, USA, July 1989.
12. Hibbit, Karlsson & Sorensen, Inc. ABAQUS/Standard User’s Manual, 6.4 ed., 2003.
13. Failure analysis of bolted composite joints exhibiting in-plane failure modes10.1177/002199839603000304 ↗
14. Effect of bolt load proportioning on the capacity of multiple-bolt composite joints10.2514/3.45560 ↗
15. Three-dimensional stress analysis of bolted single-lap composite joints10.1016/S0263-8223(98)00103-2 ↗
16. Shear loaded fastener installations
17. Combined bearing and bypass loading on a graphite/epoxy laminate10.1016/0263-8223(86)90066-8 ↗
18. Failure analysis of bolted joints in composite laminates
19. Two-dimensional modeling of composite pinned-joint failure10.1177/002199839502900507 ↗
20. McCarthy MA, McCarthy CT. Three-dimensional finite element analysis of single-bolt, single-lap composite bolted joints: part 2-effects of bolt-hole clearance. Compos Struct 2005; in press. Available online 10 November 2004.10.1016/j.compstruct.2004.09.023 ↗
21. Finite element analysis of the effects of clearance on single-shear, composite bolted joints
22. McCarthy MA, McCarthy CT, Lawlor VP, Stanley WF. Three-dimensional finite element analysis of single-bolt, single-lap composite bolted joints: part 1-model development and validation. Compos Struct 2005; in press. Available online 5 November 2004.10.1016/j.compstruct.2004.09.024 ↗
23. Palmberg B. Instrumented bolts for measurements of their shear load transfer in single and double shear joints. Technical report, The Aeronautical Research Institute of Sweden, 1991. FFA TN 1991-09.
24. Bearing failure analysis of mechanically fastened joints in composite laminates10.1016/S0263-8223(01)00004-6 ↗
25. Coefficient of friction for Aluminium in contact with a carbon fiber epoxy composite10.1016/j.triboint.2003.11.008 ↗
26. The behavior of single-lap bolted joints in CFRP laminates10.1016/0263-8223(86)90067-X ↗
27. Measurement of load distribution in multi-bolt, composite joints, in the presence of varying clearance10.1179/146580102225006512 ↗