Journals
Publish with us
Publishing partnerships
About us
Blog
Shock and Vibration
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
Shock and Vibration
/
2016
/
Article
/
Fig 14
/
Research Article
Geometrically Nonlinear Aeroelastic Stability Analysis and Wind Tunnel Test Validation of a Very Flexible Wing
Figure 14
Torsional angle of the wing spar spanwise (0.5° AOA, 34 m/s).