Flutter assessment on composite plate with crack by means of fully coupled Finite Element and Doublet Lattice Method

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Flutter assessment on composite plate with crack by means of fully coupled Finite Element and Doublet Lattice Method

This paper presents an investigation on flutter behaviour of composite plate with crack. This work is divided into two sections; (a) variation of crack length at a fix location on the plate, (b) variation of crack location on the plate with a fix crack length. The composite plate is modelled as unid...

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Bibliographic Details
Main Authors:	Abdullah, Nur Azam, Curiel-Sosa, Jose Luis, Akbar, Mahesa
Format:	Proceeding Paper
Language:	English English
Published:	2017
Subjects:	TL500 Aeronautics TL787 Astronautics
Online Access:	http://irep.iium.edu.my/74972/ http://irep.iium.edu.my/74972/1/mechcomp-2nd%20cert.pdf http://irep.iium.edu.my/74972/7/74972%20Flutter%20assessment.pdf

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