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° while the outboard sweep angle is 35°. In addition, the Boomerang...

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Bibliographic Details
Published in:	Journal of Aeronautics, Astronautics and Aviation
Main Author:	Mutaali A.B.A.; Noryatim A.N.M.; Nasir R.E.M.; Hamid A.H.A.; Mokhtar A.S.
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-s2.0-85187540571&doi=10.6125%2fJoAAA.202403_56%281S%29.21&partnerID=40&md5=e32e0ff5fdff2f590aa4c3be39764403

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