Design Analysis and Experimental Modal Testing of a Mission Adaptive Wing of an Unmanned Aerial Vehicle

Date

2010-06-10

Author

Şahin, Melin
Evren, Sakarya
Ünlüsoy, Levent
Erdoğan Tolga, İnsuyu
Güçlü, Seber
Özgen, Serkan
Yaman, Yavuz

Metadata

Show full item record

Item Usage Stats

6
views

0
downloads

Cite This

The mission adaptive wings aim to overcome the inefficient behaviour of the classical fixed wings, especially for the off-design conditions, by changing their geometry actively to adopt to changing flight conditions for maximized performance. This study presents the structural design, analysis and experimental modal testing of an unmanned aerial vehicle wing having mission adaptive characteristics.

URI

https://hdl.handle.net/11511/73736
http://www.ae.metu.edu.tr/~yyaman/LabCapabilities/Appendix/Papers/International/Conference/AAECTTUAVMAW_ICP_3.pdf

Collections

Department of Aerospace Engineering, Conference / Seminar