Finite element analysis of laminated composite plates.
MetadataShow full item record
A bi-quadratic isoparametric plate/shell bending finite element is developed to study the behavior of isotropic and laminated composite plates. The element is based on Mindlin-Reissner's theory and the principle of virtual displacements. The element is implemented in a computer program. Results are presented and compared with analytical solutions to validate this element. Good agreement is observed for thin plates, while discrepancies are noted for thick plates. Effects of various integration schemes on the element performance are presented. Convergence studies for laminated composites for different fiber orientations are also discussed.
RightsCopyright is reserved by the copyright owner
Showing items related by title, author, creator and subject.
Alon, Yair (Monterey, California: Naval Postgraduate School, 1990);A triquadratic isoparametric solid element is developed to study the behavior of thick isotropic and laminated composite plates. The element is a 27 noded Lagrangian element based on three dimensional elasticity. Material ...
Elshafei, Mostafa Adnan (Monterey, California. Naval Postgraduate School, 1996-09);In the present work, the shape control of fiber reinforced composite plate with embedded piezoelectric actuators is investigated. A finite element formulation is developed for modeling a laminated composite plate that has ...
Aygunes, Haluk (Monterey, California. Naval Postgraduate School, 1994);A new finite element modeling is presented to investigate the static and dynamic behavior of laminated composite beams with partial delamination. In this study, a newly developed rectangular beam element is used. The element ...