Modeling And Analysis Of Composite Hinge For Aircraft Spoiler Using Finite Element Analysis

This thesis is concerned with the modeling and analysis of a composite hinge bracket for Airbus A320 aircraft using Finite Element Method. The increasing demand of composite materials in aircraft structural design is due to the high strength and stiffness to weight ratio of the composite materials....

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Détails bibliographiques
Auteur principal:	Wai, Chee Mun
Format:	Thèse
Langue:	anglais anglais
Publié:	2014
Sujets:	TJ Mechanical engineering and machinery
Accès en ligne:	http://eprints.utem.edu.my/id/eprint/15010/ https://plh.utem.edu.my/cgi-bin/koha/opac-detail.pl?biblionumber=92071
Abstract	Abstract here

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