Due to their inherent advantages over mechanical-fastening methods, the use of adhesively bonded composite joints has been significantly increased in recent years for joining composite beams, panels, tubes, etc., which are fundamental components in civilian, military and aeronautic structures. Because the applied load in the adherends is always transferred in the form of shear and/or peel stresses through the adhesive layer, the stress concentration developed in the end regions at the adhesive bondline is the principal ...
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Due to their inherent advantages over mechanical-fastening methods, the use of adhesively bonded composite joints has been significantly increased in recent years for joining composite beams, panels, tubes, etc., which are fundamental components in civilian, military and aeronautic structures. Because the applied load in the adherends is always transferred in the form of shear and/or peel stresses through the adhesive layer, the stress concentration developed in the end regions at the adhesive bondline is the principal reason for causing the premature and catastrophic failure of adhesively bonded joints. This has always been a dilemma for the designers of such joints. In order to reduce the peel/shear stresses concentration and improve the joint strength, some traditional mechanical methods have been developed as practical solutions to reduce the stress concentration, such as rounding off sharp edges, spewing fillets, and tapering adherends. These methods are passive in reducing stress concentration, i.e., they are ineffective unless the pattern and magnitude of the applied loads are fixed. Comparing to these traditional mechanical enhancement methods, an active smart strength improvement method for adhesively bonded composite joint is introduced in this book to adaptively realise the reduction of peel/shear stress concentration through the integrated piezoelectric layers as sensor/actuator in the composite joint system.
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