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...

תיאור מלא

מידע ביבליוגרפי

Main Authors:	Jahangir Alam, Wing Commander G.M., Mamun, Dr. Md., Abu. Taher Ali, Dr. Md., Sadrul Islam, Dr. A. K. M.
פורמט:	Article
שפה:	אנגלית
יצא לאור:	R&D Wing, MIST 2015
נושאים:	Unmanned Air Vehicles (UAV), Aerofoil Shaped Fuselage, Aerodynamic Characteristics, Lift Coefficient, Drag Coefficient
גישה מקוונת:	http://hdl.handle.net/123456789/221
תגים:	הוספת תג אין תגיות, היה/י הראשונ/ה לתייג את הרשומה!