Development Of Design Of Aerofoil Shaped Fuselage And CFD Investigation Of Its Aerodynamic Characteristics

This paper explains about the computational design procedure for designing of an Unmanned Air Vehicles (UAV) having “Aerofoil Shaped Fuselage”. It also explains and analyses of the aerodynamic characteristics of an “Aerofoil Shaped Fuselage”. This model could be used for designing of the future UAV...

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Manylion Llyfryddiaeth

Prif Awduron:	Jahangir Alam, Wing Commander G.M., Mamun, Dr. Md., Abu. Taher Ali, Dr. Md., Sadrul Islam, Dr. A. K. M.
Fformat:	Erthygl
Iaith:	Saesneg
Cyhoeddwyd:	R&D Wing, MIST 2015
Pynciau:	Unmanned Air Vehicles (UAV), Aerofoil Shaped Fuselage, Aerodynamic Characteristics, Lift Coefficient, Drag Coefficient
Mynediad Ar-lein:	http://hdl.handle.net/123456789/221
Tagiau:	Ychwanegu Tag Dim Tagiau, Byddwch y cyntaf i dagio'r cofnod hwn!