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Modulus reduction and fatigue damage of matrix dominated composite laminates

✍ Scribed by J.N. Yang; L.J. Lee; D.Y. Sheu

Book ID
107934077
Publisher
Elsevier Science
Year
1992
Tongue
English
Weight
820 KB
Volume
21
Category
Article
ISSN
0263-8223

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The effect of the fibre pattern on the tension fatigue properties of z-pinned composite laminates is experimentally investigated. Carbon-epoxy laminates with fibre-dominated ([0] 20 and [0/Β±45/90] 5s ) and matrix-dominated ([Β±45] 10s ) ply patterns were reinforced in the through-thickness direction