Exact(44)
However, current analysis methods and empirical databases for composite bonded joint design and composite bonded patch repair are limited to flat plate and/or flat laminate geometries, and the effects of curvature on the performance and durability of composite bonded joints and repairs is not known.
This paper presents a two-dimensional finite element analysis of composite bonded single-lap joints.
Failure analysis of composite bonded repairs in cracked metallic structures is often given superficial treatment.
Composite bonded joints are prone to disbond when submitted to fatigue or extreme loads.
Current practice to design aircraft composite bonded joints only allows a non-growth certification approach for failure.
Based on these findings, specific suggestions for the enhancement of composite bonded repairs against debonding are made.
Similar(16)
In the present study, single lap metal-composite bonded joints of titanium and CFRP parts were manufactured by using an epoxy adhesive film.
Based on the experimental set-up shown by the Figure 4, it was investigated the vibration-based damage identification for metal-composite bonded joints.
A damage identification experimental study was shown for single lap metal-composite bonded joint made of titanium and epoxy resin reinforced by carbon fiber.
Figure 1 Experimental model: (a) single lap metal-composite bonded joint with accelerometer and piezoelectric transducer attached to the titanium part and (b) important dimensions.
Borges (2012) investigated experimentally and numerically via the vibration-based method the changes in a metal-composite bonded joint by using piezoelectric patch and accelerometers in order to monitor the damage in the joint.
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