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Medientyp:
E-Artikel
Titel:
A Boundary Layer Approach to Interlaminar Stresses in Composite Laminates with Curved Edges
Beteiligte:
Lin Ye;
Yang, Bing-Xian
Erschienen:
SAGE Publications, 1988
Erschienen in:
Journal of Reinforced Plastics and Composites, 7 (1988) 2, Seite 179-198
Sprache:
Englisch
DOI:
10.1177/073168448800700207
ISSN:
0731-6844;
1530-7964
Entstehung:
Anmerkungen:
Beschreibung:
A way for determining the interlaminar stresses in composite laminates with arbitrary curved edges is described using the boundary layer equations. A simple and efficient method for the calculation of interlaminar stresses is presented. The method gives a stress field that satisfies the zeroth order equilibrium equations and the stress boundary condi tions as well as the stress continuity between plies. Several laminates with a circular hole are dealt with by the present method. The results indicate that the method is of great versatility and has the ability to perform the analysis of thick laminates efficiently.