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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Hlavní autoři:	Jahangir Alam, Wing Commander G.M., Mamun, Dr. Md., Abu. Taher Ali, Dr. Md., Sadrul Islam, Dr. A. K. M.
Médium:	Článek
Jazyk:	angličtina
Vydáno:	R&D Wing, MIST 2015
Témata:	Unmanned Air Vehicles (UAV), Aerofoil Shaped Fuselage, Aerodynamic Characteristics, Lift Coefficient, Drag Coefficient
On-line přístup:	http://hdl.handle.net/123456789/221
Tagy:	Přidat tag Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!