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Stress-strain analysis of an adhesive-bonded taper-taper joint between two composite flat plates

Helms, Jack E.
Yang, Chihdar Charles
Pang, Su-Seng
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1996-05
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Conference paper
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Keywords
Adhesive joints,Adhesion,Computer software,Finite element method,Mathematical models,Plates (structural components),Shear deformation,Stress analysis,Composite flat plates,Laminate plate theory,Software package COSMOS/M
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Helms, J. E., Yang, C., & Pang, S. (1996). Stress-strain analysis of an adhesive-bonded taper-taper joint between two composite flat plates. Paper presented at the Annual Technical Conference - ANTEC, Conference Proceedings, , 1 1297-1301.
Abstract
An analytical model of a taper-taper adhesive-bonded joint between two composite flat plates has been developed using classical first-order laminated plate theory and including a correction for transverse shear deformation effects. The model was derived under the assumption of plane stress in the adherends. The model consists of eighteen first-order, coupled ordinary differential equations with non-constant coefficients. The model was solved numerically. A finite element model was also developed to verify the results of the analytical model using the COSMOS/M commercial software package.
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Society of Plastics Engineers (SPE)
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Annual Technical Conference, ANTEC
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