Modeling of adaptive composites including debonding
β Scribed by Charles E. Seeley; Aditi Chattopadhyay
- Publisher
- Elsevier Science
- Year
- 1999
- Tongue
- English
- Weight
- 555 KB
- Volume
- 36
- Category
- Article
- ISSN
- 0020-7683
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β¦ Synopsis
Debonding of piezoelectric actuators for use in composite structures can result in signi_cant changes to the static and dynamic response[ This important issue is studied in the current work[ The re_ned higher order theory for composite laminates with embedded:surface bonded piezoelectric sensors and actuators is extended to incorporate debonding of transducers by partitioning the laminate into debonded and non! debonded regions[ The stress free boundary conditions at the free surfaces are satis_ed in the analytical formulation[ Continuity conditions between the debonded and the nondebonded regions\ which are non! trivial for the higher order theory\ are formulated and implemented using a penalty approach in the _nite element model[ The computational model is e.cient and correlation with experimental results is very good[ Numerical results are presented which indicate signi_cant changes in the natural frequencies and mode shapes due to debonded transducers[ Γ 0887 Elsevier Science Ltd[ All rights reserved
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Experimental studies on the failure mode of composite T-joint specimens, in the presence of adhesive interlaminar layers, are presented. Tests underline the role played by the interaction between delamination and debonding phenomena. Quasi static analyses of the tests are performed by means of expli
A laminated composite may fail by various mechanisms: debonding, delamination, fiber fracture, matrix cracking, and fiber buckling. The fiber fracture possess the greatest threat the structure integrity. However, the progressive debonding often increases the load sustained by the fiber; therefore, i