Journals
Publish with us
Publishing partnerships
About us
Blog
Complexity
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
Complexity
/
2020
/
Article
/
Fig 6
/
Research Article
Optimization of Fuel Injection Control System of Two-Stroke Aeroengine of UAV
Figure 6
Dynamic displacement of the needle valve with different spring initial tension
F
0
. (a)
F
0
= 5.5 N. (b)
F
0
= 9.5 N. (c)
F
0
= 8.0 N.
(a)
(b)
(c)