A simple 2D boundary element analysis, suitable for developing cost effective models for tapered composite laminates, is presented. Constant stress and displacement elements are used. Closed-form fundamental solutions are derived. Numerical results are provided for several configurations to illustrate the accuracy of the model.
Simple boundary element analysis of laminated composite structures
2001
10 Seiten, 9 Quellen
Conference paper
English
AIAA-2001-1544 Simple Boundary Element Analysis of Laminated Composite Structures
British Library Conference Proceedings | 2001
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