Improved transverse shear stresses in composite finite elements based on first order shear deformation theory

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  • German Aerospace Center (DLR) (e.V.) Location Braunschweig
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Details

Original languageEnglish
Pages (from-to)51-60
Number of pages10
JournalInternational Journal for Numerical Methods in Engineering
Volume40
Publication statusPublished - 4 Dec 1998
Externally publishedYes

Abstract

A method for calculating improved transverse shear stresses in laminated composite plates, which bases on the first-order shear deformation theory is developed. In contrast to many recently established methods, either higher-order lamination theories or layerwise theories, it is easily applicable to finite elements, since only C0-continuity is necessary and the numerical effort is low. The basic idea is to calculate the transverse shear stresses directly from the transverse shear forces by neglecting the influence of the membrane forces and assuming two cylindrical bending modes. Shear correction factors are no longer required, since the transverse shear stiffnesses are also provided. Numerical examples for symmetric cross-ply and antisymmetric angle-ply laminates show the superiority of the method against using shear correction factors. Furthermore, results obtained with MSC/NASTRAN, which uses a similar but simplified approach, are surpassed.

Keywords

    Fiber composite, Finite shell elements, Interlaminar shear, Laminate, Shear deformation theory, Transverse shear stiffness

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Improved transverse shear stresses in composite finite elements based on first order shear deformation theory. / Rolfes, R.; Rohwer, K.
In: International Journal for Numerical Methods in Engineering, Vol. 40, 04.12.1998, p. 51-60.

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AU - Rolfes, R.

AU - Rohwer, K.

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