Journals
Publish with us
Publishing partnerships
About us
Blog
Mathematical Problems in Engineering
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
Mathematical Problems in Engineering
/
2021
/
Article
/
Fig 12
/
Research Article
Effect of Stiffness on Flutter of Composite Wings with High Aspect Ratio
Figure 12
Time response histories under 0.5 Ma. (a)
= 217.3 m/s, (b)
= 228.9 m/s, and (c)
= 248.2 m/s.
(a)
(b)
(c)