Limit Cycle Oscillation (LCO) flutter of advanced high modulus graphite/epoxy composite oscillating supersonic wing

• Main Authors: Abdullah, Nur Azam, Sulaeman, Erwin, Ahmad, Meor iqram Meor
• Format: Conference or Workshop Item
• Language: English; English
• Published: 2021
• Subjects: T175 Industrial research. Research and development; TJ170 Mechanics applied to machinery. Dynamics; TJ181 Mechanical movements; TJ227 Machine design and drawing; TJ241 Machine construction (General); U Military Science (General)
• Online Access: http://irep.iium.edu.my/88907/2/Extended%20Abstract%20-LCO.pdf; http://irep.iium.edu.my/88907/13/88907_Limit%20Cycle%20Oscillation%20%28LCO%29.pdf; http://irep.iium.edu.my/88907/
• Institution: Universiti Islam Antarabangsa Malaysia

This paper presents an optimisation process of reducing the structural weight of the supersonic wing by constraining the structural durability due to limit cycle oscillation. The application of composite material in aeroelasticity contributes to the modification of the expected aeroelastic failure o...