Aerodynamic design and characterization of a quad tilt-wing UAV via wind tunnel tests

Çetinsoy, Ertuğrul and Hançer, Cevdet and Öner, Kaan Taha and Sırımoğlu, Efe and Ünel, Mustafa (2011) Aerodynamic design and characterization of a quad tilt-wing UAV via wind tunnel tests. (Accepted/In Press)

There is a more recent version of this item available.

Full text not available from this repository.

Official URL: http://www.asce.org/Journal.aspx?id=2147486559

Item Type:	Article
Uncontrolled Keywords:
Subjects:	T Technology > TJ Mechanical engineering and machinery T Technology > TK Electrical engineering. Electronics Nuclear engineering T Technology > TL Motor vehicles. Aeronautics. Astronautics
ID Code:	18616
Deposited By:	Mustafa Ünel
Deposited On:	23 Dec 2011 14:45
Last Modified:	18 Nov 2012 21:40

Available Versions of this Item

Aerodynamic design and characterization of a quad tilt-wing UAV via wind tunnel tests. (deposited 23 Dec 2011 14:45) [Currently Displayed]
- Aerodynamic design and characterization of a quad tilt-wing UAV via wind tunnel tests. (deposited 18 Nov 2012 21:40)

Repository Staff Only: item control page