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Prediction of fatigue life for matrix-dominated composite laminates

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


Book ID
107935178
Publisher
Elsevier Science
Year
1993
Tongue
English
Weight
608 KB
Volume
46
Category
Article
ISSN
0266-3538

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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/ยฑ45/90] 5s ) and matrix-dominated ([ยฑ45] 10s ) ply patterns were reinforced in the through-thickness direction