Journals
Publish with us
Publishing partnerships
About us
Blog
International Journal of Aerospace Engineering
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
International Journal of Aerospace Engineering
/
2017
/
Article
/
Fig 13
/
Research Article
Tendon-Sheath Mechanisms in Flexible Membrane Wing Mini-UAVs: Control and Performance
Figure 13
Test rigs: (a) the rigid wing and (b) the FMW model, suspended in the middle of the test section of the wind tunnel.
(a)
(b)