LCO flutter instability on oscillating supersonic wing by means of linearized aerodynamic small disturbance theory
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...
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Main Authors: | Abdullah, Nur Azam, Sulaeman, Erwin, Ahmad, Meor Iqram Meor |
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Format: | Book Chapter |
Language: | English English |
Published: |
Springer Nature Switzerland AG
2022
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Subjects: | |
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 |
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