Aerodynamics Analysis of a Boomerang Blended-Wing-Body Unmanned Aerial Vehicle using Different Numerical Simulation Tools

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Aerodynamics Analysis of a Boomerang Blended-Wing-Body Unmanned Aerial Vehicle using Different Numerical Simulation Tools

Boomerang blended -wing -body (BWB) is a compound wing consisting of inboard and outboard wings that resembles the shape of a boomerang. For the focused Boomerang BWB unmanned aerial vehicle (UAV) design, the inboard sweep angle is 40 degrees while the outboard sweep angle is 35 degrees. In addition...

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Bibliographic Details
Published in:	JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION
Main Authors:	Muta'ali, Atikah Basyirah Abdul; Noryatim, Ahmad Norsyamiel Mohamad; Nasir, Rizal Effendy Mohd; Hamid, Ahmad Hussein Abdul; Mokhtar, Azib Syahmi
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:001278413400001

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