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

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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 inboar...

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Bibliographic Details
Published in:	JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION
Main Authors:	Osman, Azraai; Hamid, Ahmad Hussein Abdul; Yusof, Muhammad Fida'iy Najmie Mohamed; Nasir, Rizal Effendy Mohd
Format:	Article
Language:	English
Published:	AERONAUTICAL & ASTRONAUTICAL SOC REPUBLIC CHINA 2024
Subjects:	Engineering
Online Access:	https://www-webofscience-com.uitm.idm.oclc.org/wos/woscc/full-record/WOS:001278415000001

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