Please use this identifier to cite or link to this item:
|Title:||Assumed strain quadrilateral C0 laminated plate element based on third-order shear deformation theory|
|Source:||Shi, G.,Lam, K.Y.,Tay, T.E.,Reddy, J.N. (1999-12). Assumed strain quadrilateral C0 laminated plate element based on third-order shear deformation theory. Structural Engineering and Mechanics 8 (6) : 623-637. ScholarBank@NUS Repository.|
|Abstract:||This paper presents a four-noded quadrilateral C0 strain plate element for the analysis of thick laminated composite plates. The element formulation is based on: 1) the third-order shear deformation theory; 2) assumed strain element formulation; and 3) interrelated edge displacements and rotations along element boundaries. Unlike the existing displacement-type composite plate elements based on the third-order theory, which rely on the C1-continuity formulation, the present plate element is of C0-continuity, and its element stiffness matrix is evaluated explicitly. Because of the third-order expansion of the in-plane displacements through the thickness, the resulting theory and hence elements do not need shear correction factors. The explicit element stiffness matrix makes the present element more computationally efficient than the composite plate elements using numerical integration for the analysis of thick layered composite plates.|
|Source Title:||Structural Engineering and Mechanics|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Feb 17, 2018
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.