Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
6707588 | Composite Structures | 2014 | 16 Pages |
Abstract
This paper presents an analysis method for the determination of displacements, strains and stresses in a laminated composite plate subjected to tensile load that is reinforced by a doubler. The analysis approach consists of two parts. Firstly, a 'global' solution that is based on Classical Laminated Plate Theory (CLPT) is introduced. Secondly, a 'local' model is derived that enables the assessment of the three-dimensional stress state near the plate-doubler junction. The local solution employs a discretization of the physical layers into a number of mathematical layers which necessitates the numerical treatment of a quadratic eigenvalue problem. Consequently, the current approach can be classified as being a semi-analytical layerwise analysis method. Results are generated for several different plate-doubler configurations, and it is found that the current analysis model delivers excellent results when compared to finite element simulations, however with only a fraction of the computational time and effort that are needed for the FEM analyses.
Related Topics
Physical Sciences and Engineering
Engineering
Civil and Structural Engineering
Authors
Jan Eike Butzke, Christian Mittelstedt,