Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM

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Structural integrity assessment of cracked composite plate under aeroelastic loading by means of XFEM

In this paper, a novel procedure to analyse dynamic crack under aeroelastic loading by means of XFEM and Doublet Lattice Method (DLM) - FEM coupling is presented. The present work performed a new investigation on the crack propagation on the composite plate exerted by the unsteady aerodynamic loadi...

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Bibliographic Details
Main Authors:	Abdullah, Nur Azam, Curiel-Sosa, J.L., Wirawan, Nanda, Akbar, Mahesa
Format:	Proceeding Paper
Language:	English English
Published:	2018
Subjects:	TL500 Aeronautics TL787 Astronautics
Online Access:	http://irep.iium.edu.my/74973/ http://irep.iium.edu.my/74973/1/7207.pdf http://irep.iium.edu.my/74973/7/74973_Program.pdf

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