Aerodynamic Evaluation of UiTM’s Blended Wing Body Unmanned Aerial Vehicle at Different Elevon Configurations using Vortex Lattice Method

Aerodynamic Evaluation of UiTM’s Blended Wing Body Unmanned Aerial Vehicle at Different Elevon Configurations using Vortex Lattice Method

This paper presents findings of the preliminary aerodynamic evaluation for UiTM’s baseline model blended wing body (BWB) unmanned aerial vehicle (UAV). The UAV design is based on a new planform and hence its characteristics were yet to be understood. The design is tailless, with both the inboard and...

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Bibliographic Details
Published in:Journal of Aeronautics, Astronautics and Aviation
Main Author: Osman A.; Hamid A.H.A.; Yusof M.F.N.M.; Nasir R.E.M.
Format: Article
Language:English
Published: The Aeronautical and Astronautical Society of the Republic of China 2024
Online Access:https://www.scopus.com/inward/record.uri?eid=2-s2.0-85187552781&doi=10.6125%2fJoAAA.202403_56%281S%29.30&partnerID=40&md5=ce3acf3fabc34241c139393c6bcdfa2f

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https://www.scopus.com/inward/record.uri?eid=2-s2.0-85187552781&doi=10.6125%2fJoAAA.202403_56%281S%29.30&partnerID=40&md5=ce3acf3fabc34241c139393c6bcdfa2f

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