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

• 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/73583/7/73583%20Aeroelastic%20assessment%20of%20cracked%20composite.pdf; http://irep.iium.edu.my/73583/8/73583%20Aeroelastic%20assessment%20of%20cracked%20composite%20SCOPUS.pdf; http://irep.iium.edu.my/73583/; https://www.sciencedirect.com/science/article/pii/S026382231733266X

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...