Application of Failure Criteria in Aeronautical Sandwich Structure Composites with a Central Hole Subjected to Bending Testing

Application of Failure Criteria in Aeronautical Sandwich Structure Composites with a Central Hole Subjected to Bending Testing

Abstract This study aimeds at investigating the mechanical behavior of an E-glass fiber-reinforced epoxy resin of a laminated composite sandwich with honeycomb core and a central hole, used in the aeronautics industry submitted to bending loading. Three analytical failure models applied to laminated...

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Bibliographic Details
Main Authors: Franciélio Gomes da Silva, Raimundo Carlos Silverio Freire Júnior, Selma Hissae Shimura da Nobrega, Avelino Manuel da Silva Dias
Format: Article
Language:English
Published: Associação Brasileira de Metalurgia e Materiais (ABM); Associação Brasileira de Cerâmica (ABC); Associação Brasileira de Polímeros (ABPol) 2020-06-01
Series:Materials Research
Subjects:
Aeronautical Sandwich Composites
Failures Models
Bending Test
Online Access:http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392020000200216&tlng=en

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