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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主要な著者:	Jahangir Alam, Wing Commander G.M., Mamun, Dr. Md., Abu. Taher Ali, Dr. Md., Sadrul Islam, Dr. A. K. M.
フォーマット:	論文
言語:	英語
出版事項:	R&D Wing, MIST 2015
主題:	Unmanned Air Vehicles (UAV), Aerofoil Shaped Fuselage, Aerodynamic Characteristics, Lift Coefficient, Drag Coefficient
オンライン･アクセス:	http://hdl.handle.net/123456789/221
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