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Technical Paper

An Investigation on the Fatigue Behavior of Balanced and Unbalanced Epoxy-Aluminum Single Lap Joints

2015-04-14
2015-01-0551
The fatigue strength and failure behavior of A5754-O adhesively bonded single lap joints by a hot-curing epoxy adhesive were investigated in this paper. The single lap joints tested include balanced substrate joints (meaning same thickness) and unbalanced substrate joints, involving combinations of different substrate thicknesses. Cyclic fatigue test results show that the fatigue strength of bonded joints increase with the increasing substrate thickness. SEM and Energy Dispersive X-ray (EDX) were employed to investigate the failure mode of the joints. Two fatigue failure modes, substrate failure and failure within the adhesive were found in the testing. The failure mode of the joint changes from cohesive failure to substrate failure as the axial load is decreased, which reveals a fatigue resistance competition between the adhesive layer and the aluminum substrate.
Journal Article

Finite Element Modeling of Dissimilar Metal Self-piercing Riveting Process

2014-04-01
2014-01-1982
In present paper, the process of joining aluminum alloy 6111T4 and steel HSLA340 sheets by self-piercing riveting (SPR) is studied. The rivet material properties were obtained by inverse modeling approach. Element erosion technique was adopted in the LS-DYNA/explicit analysis for the separation of upper sheet before the rivet penetrates into lower sheet. Maximum shear strain criterion was implemented for material failure after comparing several classic fracture criteria. LS-DYNA/implicit was used for springback analysis following the explicit riveting simulation. Large compressive residual stress was observed near frequent fatigue crack initiation sites, both around vicinity of middle inner wall of rivet shank and upper 6111T4 sheet.
Technical Paper

Stress Intensity Factor Based Spot Welds Fatigue Life Prediction Model

2013-04-08
2013-01-0389
The present paper focuses on fatigue modeling of resistance spot-welded (RSW) joints. Fatigue tests are performed on aluminum RSW joints and fatigue data are generated. Stress intensity factors at nugget circumference are calculated based on loads transferred by weld nugget. An equivalent stress intensity factor Keq is defined and modified to correlate fatigue test results. Keq modified by critical crack length is proven efficient in consolidating a large amount of fatigue data with correlation result significantly improved. Practical potentiality of this model in automobile body structure fatigue analysis is discussed. The proposed model could be readily applied to structure fatigue analysis.
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