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Muhammad Fida'iy Najmie Mohamed; Nasir
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Aerodynamic Evaluation of UiTM's Blended Wing Body Unmanned Aerial Vehicle at Different Elevon Configurations using Vortex Lattice Method
by
Osman
,
Azraai; Hamid
,
Ahmad Hussein Abdul; Yusof
,
Muhammad
Fida'iy
Najmie
Mohamed
;
Nasir
,
Rizal Effendy Mohd
Published in
JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION
(2024)
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