Computational aerodynamic analysis of UiTM's Hawkeye UAV aircraft
This paper discusses the aerodynamic characteristics of Hawkeye UAV aircraft with a forward-swept wing configuration. The unconventional wing design on Hawkeye allows for better maneuverability and stability during a field test but there were no prior studies on its aerodynamic characteristics. A se...
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Main Authors: | Johari, M. Syazwan, M. Ali, Zurriati, Wisnoe, Wirachman, Ismail, Noriswadi, Ishak, Iskandar S. |
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Format: | Article |
Published: |
The Aeronautical and Astronautical Society of the Republic of China
2021
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Subjects: | |
Online Access: | http://eprints.utm.my/id/eprint/95245/ http://dx.doi.org/10.6125/JoAAA.202106_53(2).23 |
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