LCO flutter instability on oscillating supersonic wing by means of linearized aerodynamic small disturbance theory

• Main Authors: Abdullah, Nur Azam, Sulaeman, Erwin, Ahmad, Meor Iqram Meor
• Format: Book Chapter
• Language: English; English
• Published: Springer Nature Switzerland AG 2022
• Subjects: T175 Industrial research. Research and development; T351 Mechanical drawing. Engineering graphics; TJ170 Mechanics applied to machinery. Dynamics; TJ181 Mechanical movements; TJ210.2 Mechanical devices and figures. Automata. Ingenious mechanism. Robots (General); U Military Science (General)
• Online Access: http://irep.iium.edu.my/96552/1/96552_LCO%20flutter%20instability%20on%20oscillating%20supersonic%20wing.pdf; http://irep.iium.edu.my/96552/7/96552_LCO%20flutter%20instability%20on%20oscillating%20supersonic%20wing_Scopus.pdf; http://irep.iium.edu.my/96552/; https://link.springer.com/book/10.1007/978-3-030-85646-5

This article offers an optimization procedure in designing much lighter supersonic wing by employing a composite structure by constraining the structural persistence due to flutter speed, a type of aeroelasticity failure. The application of composite material in aeroelasticity contributes to the ch...