Mechanical performance of carbon-epoxy laminates. Part I: quasi-static and impact bending properties

In Part I of this study, quasi-static and impact bending properties of four aeronautical grade carbon-epoxy laminates have been determined and compared. Materials tested were unidirectional cross-ply (tape) and bidirectional woven textile (fabric) carbon fiber lay-up architectures, impregnated with...

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Bibliographic Details
Main Authors: José Ricardo Tarpani, Marcelo Tadeu Milan, Dirceu Spinelli, Waldek Wladimir Bose
Format: Article
Language:English
Published: Associação Brasileira de Metalurgia e Materiais (ABM); Associação Brasileira de Cerâmica (ABC); Associação Brasileira de Polímeros (ABPol) 2006-06-01
Series:Materials Research
Subjects:
Online Access:http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392006000200002