Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method

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Aeroelastic assessment of cracked composite plate by means of fully coupled finite element and Doublet Lattice Method

This paper presents an investigation on flutter speed of cracked composite plates. This work is divided into two sections: (a) variation of crack length at a fixed location on the plate, and (b) variation of crack location on the plate with a fixed crack length, modelled as a unidirectional compos...

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Bibliographic Details
Main Authors:	Abdullah, Nur Azam, Curiel-Sosa, Jose Luis, Akbar, Mahesa
Format:	Article
Language:	English English
Published:	Elsevier 2018
Subjects:	QC Physics T Technology (General) T175 Industrial research. Research and development TJ1425 Lifting and pressing machinery TJ170 Mechanics applied to machinery. Dynamics
Online Access:	http://irep.iium.edu.my/73583/ http://irep.iium.edu.my/73583/7/73583%20Aeroelastic%20assessment%20of%20cracked%20composite.pdf http://irep.iium.edu.my/73583/8/73583%20Aeroelastic%20assessment%20of%20cracked%20composite%20SCOPUS.pdf

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