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
/
2019
/
Article
/
Tab 1
/
Research Article
The Effect of Damping Coefficient, Spring Coefficient, and Mass Ratio on the Power Extraction Performance of a Semiactive Flapping Wing
Table 1
Parameters considered in this paper.
Damping coefficient
Spring coefficient
Mass ratio
0.0625~18.0
0.00~3.00
15~240