Simplified stress analysis of hybrid (bolted/bonded) joints
Source abstract
Abstract
The load transfer in hybrid (bolted/bonded) – denoted HBB – single-lap joints is complicated due to the association of two different transfer modes (discrete and continuous) through elements with different stiffnesses. The Finite Element (FE) method can be used to address the stress analysis of those joints. However, analyses based on FE models are computationally expensive and it would be profitable to use simplified approaches enabling extensive parametric studies. Two among the authors of this paper participated in the development of a dedicated 1D-beam approach (Paroissien 2007). This paper presents an extension of this framework enabling (i) the analysis of HBB joints made of dissimilar laminated or monolithic adherends, and (ii) the introduction of non linear material behaviour for both the adhesive layer and the fasteners. The output data are the distributions of displacements and forces in the adherends and fasteners, as well as those of adhesive shear and peeling stresses, allowing for a fast assessment of the material behaviour and strength prediction of HBB joints. The use of this model is illustrated in the identification of the failure mechanisms of HBB joints under quasistatic loadings, based on experimental and numerical tests on single-lap HBB joint. It is worth mentioning that the model can support pure bonded and pure bolted configurations. It can be used during the presizing phase at the design office (possibly independently on commercial software), to obtain quickly mechanical performances and to help in decision making. Moreover, it was shown that the judicious choice of the adhesive material allows for a significant increase of the static and fatigue strength compared to pure bolted or bonded corresponding configurations (Kelly 2006) (Paroissien 2006). The model can then be used to formulate at best adhesive materials to optimize the mechanical performance of HBB joints according to work specifications.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Mechanical Behavior of Composites · Structural Behavior of Reinforced Concrete · Structural Load-Bearing Analysis
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (35)
Show source-provided references
1. Damage mechanics of interfacial media: basic aspects, identification and application to delamination
2. A delay damage mesomodel of laminates under dynamic loading: basic aspects and identification issues10.1016/S0045-7949(03)00035-X ↗
3. Elastic analysis and engineering design formulae for bonded joints10.1016/0143-7496(89)90066-3 ↗
4. Measurement of mixed-mode delamination fracture. Toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus10.1016/0266-3538(96)00005-X ↗
5. An analytical model for the strength prediction of hybrid (bolted/bonded)10.1016/j.compstruct.2012.10.022 ↗
6. Static and fatigue testing thin riveted, bonded and hybrid fiber double lap joints used in aircraft structures10.1016/j.compstruct.2014.11.004 ↗
7. Cope DA, Lacy TE. Stress intensity determination in lap joints with mechanical fasteners. In: Proceedings of the 41st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials conference, AIAA-2000–1368, 3-6 April 2000, Atlanta, GA; 2000.10.2514/6.2000-1368 ↗
8. Use of J-integral as fracture parameter in simplified analysis of bonded joints10.1007/BF00053316 ↗
9. Fatigue of hybrid (adhesive/bolted) joints in SRIM composites10.1016/S0143-7496(00)00047-6 ↗
10. The stresses in cemented joints10.1115/1.4009336 ↗
11. Hartman A. Fatigue tests on single lap joints in clad 2024-T3 aluminium alloy manufactured by a combination of riveting and adhesive bonding. Report M.2170, NLR; 1966.
12. Hart-Smith · 1982
13. Simulation of single-lap bonded and hybrid (bolted/bonded) joints with flexible adhesive10.1016/j.ijadhadh.2009.12.002 ↗
14. Högberg · 2004
15. H Huth. Influence of Fastener flexibility on the prediction of load transfer and fatigue life for multiple row joints. Fatigue in mechanically fastened composite and metallic joints, ASTM STP 927, John M. Potter, Ed., Philadelphia, PA ; 1986. pp. 221–250.10.1520/STP29062S ↗
16. Fatigue strength of adhesive/rivet combined lap joint10.1080/00218469508014356 ↗
17. Quasi-static strength and fatigue life of hybrid (bonded/bolted) composite single-lap joints10.1016/j.compstruct.2004.11.002 ↗
18. Fatigue damage modelling of adhesively bonded joints under variable amplitude loading using a cohesive zone model10.1016/j.engfracmech.2011.09.008 ↗
19. Adding additional load paths in a bonded/bolted hybrid joint10.2514/1.C000206 ↗
20. Lachaud · 2011
21. An extended semi-analytical formulation for fast and reliable stress analysis of adhesively bonded joints10.1016/j.ijsolstr.2014.12.027 ↗
22. Analysis of adhesive bonded joints: a unified approach10.1016/S0266-3538(02)00030-1 ↗
23. Oterkus E, Barut A, Madenci E, Ambur DR. Analysis of bolted-bonded composite lap joints. In: Proceedings of the 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA-2007–2187, 23-26 April, Honolulu, Hawaii; 2007.10.2514/6.2007-2187 ↗
24. Paroissien · 2006
25. Analytical two-dimensional model of a hybrid (bolted/bonded) single-lap joint10.2514/1.24452 ↗
26. Elasto-plastic analysis of bonded joints using macro-elements10.1080/01694243.2012.745053 ↗
27. A simplified stress analysis of bonded joints using macro-elements
28. Improving load sharing in hybrid bonded/bolted composite joints using interference-fit bolt10.1016/j.compstruct.2016.04.025 ↗
29. Experimental and numerical study of fatigue crack growth of aluminium 2024-T3 single lap simple bolted and hybrid (adhesive/bolted) joints10.1016/j.engfailanal.2015.10.013 ↗
30. On the role of kinking in the bearing failure of composite laminates10.1016/j.compstruct.2016.01.058 ↗
31. Stapleton · 2012
32. T Swift. Fracture analysis of stiffened structure, Damage Tolerance of metallic structures: analysis methods and application. ASTM STP 842, J.B. Chang & J.L. Rudd, Eds., American Society for Testing and Materials, pp. 69–107; 1984.10.1520/STP32606S ↗
33. MB Tate, SJ Rosenfeld. Preliminary investigation of the loads carried by individual bolts in bolted joints. Technical Note, NACA, TN 1051; 1946.
34. A general sandwich-type model for adhesive joints with composite adherends10.1016/j.ijadhadh.2014.06.009 ↗
35. Stresses in adhesive between dissimilar adherends10.1080/00218467508075042 ↗