Analysis on cracked commuter aircraft wing under dynamic cruise load by means of XFEM

• Main Authors: Wirawan, Nanda, Abdullah, Nur Azam, Akbar, Mahesa, Curiel-Sosa, J.L.
• Format: Conference or Workshop Item
• Language: English; English; English
• Published: IOP Publishing Ltd 2018
• Subjects: TL500 Aeronautics
• Online Access: http://irep.iium.edu.my/72822/1/72822%20Analysis%20on%20Cracked%20Commuter.pdf; http://irep.iium.edu.my/72822/2/72822%20Analysis%20on%20Cracked%20Commuter%20SCOPUS.pdf; http://irep.iium.edu.my/72822/13/72822%20slides.pdf; http://irep.iium.edu.my/72822/; https://iopscience.iop.org/article/10.1088/1742-6596/1106/1/012014/pdf

In this paper, a new investigation of crack propagation on a commuter aircraft wing is discussed. The aircraft is a 19-seater multi-purpose commuter aircraft designed for a mission on the remote area. The dynamic load acting on the wing is assumed as harmonic load considering aerodynamic lift at...