Elliptical and circular bonded composite repair under mechanical and thermal loading in aircraft structures

Elliptical and circular bonded composite repair under mechanical and thermal loading in aircraft structures

In this study, the three-dimensional finite element method is used to achieve a comparison between the semi circular and semi elliptical patch repairs in aircraft structures. The comparison was done by the analysis of : the mechanical and thermal stress intensity factors (SIF and TSIF) at the tip of...

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Bibliographic Details
Main Authors: Faycal Benyahia, Abdulmohsen Albedah, Bel Abbes Bachir Bouiadjra
Format: Article
Language:English
Published: Associação Brasileira de Metalurgia e Materiais (ABM); Associação Brasileira de Cerâmica (ABC); Associação Brasileira de Polímeros (ABPol) 2014-10-01
Series:Materials Research
Subjects:
bonded composite repair
adhesive
thermal stresses
stress intensity factor
finite element method
Online Access:http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392014000500015&tlng=en

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http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1516-14392014000500015&tlng=en

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