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A platform for research: civil engineering, architecture and urbanism
Edge effects of uniformly loaded cross-ply composite laminates
AbstractInterlaminar stresses resulting from bending of rectangular cross-ply composite laminates are determined using a layer wise laminate theory. Two types of laminates are considered. First a fully simply supported laminate subjected to bi-directional bending is analyzed. The results obtained from this theory are compared with those of the published three-dimensional elasticity solutions to verify the validity and accuracy of the present theory. Then laminates with two edges simply supported and the other two edges free are examined. The results indicate the presence of significant interlaminar stresses near the free edges.
Edge effects of uniformly loaded cross-ply composite laminates
AbstractInterlaminar stresses resulting from bending of rectangular cross-ply composite laminates are determined using a layer wise laminate theory. Two types of laminates are considered. First a fully simply supported laminate subjected to bi-directional bending is analyzed. The results obtained from this theory are compared with those of the published three-dimensional elasticity solutions to verify the validity and accuracy of the present theory. Then laminates with two edges simply supported and the other two edges free are examined. The results indicate the presence of significant interlaminar stresses near the free edges.
Edge effects of uniformly loaded cross-ply composite laminates
Tahani, Masoud (author) / Nosier, Asghar (author)
2003-05-19
12 pages
Article (Journal)
Electronic Resource
English
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