Computational aerodynamic analysis of UiTM's Hawkeye UAV aircraft

• Main Authors: Johari, M. Syazwan, M. Ali, Zurriati, Wisnoe, Wirachman, Ismail, Noriswadi, Ishak, Iskandar S.
• Format: Article
• Published: The Aeronautical and Astronautical Society of the Republic of China 2021
• Subjects: TJ Mechanical engineering and machinery
• Online Access: http://eprints.utm.my/id/eprint/95245/; http://dx.doi.org/10.6125/JoAAA.202106_53(2).23
• Institution: Universiti Teknologi Malaysia

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...