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
/
2021
/
Article
/
Tab 1
/
Research Article
The Investigation on
Adaptive Control of the Tilt-Rotor Aircraft
Table 1
Basic parameters of XV-15 tilt-rotor.
Parameters value
Weight (
)
5897 kg
Rotor radius (
)
3.81 m
Blade number (
)
Blade twist (
)
-41°
Rotor speed (
)
589 rpm (helicopter mode)
517 rpm (airplane mode)
Lock number (
)
3.83
Solidity (
)
0.089
Pitch-flap coupling angle (
)
15°
Flapping hinge restraint
17476 Nm/rad
Flap moment of inertia (
)
139 kg·m
2
Nacelle length (
)
1.4 m
Wing area (
)
16.82 m
2
Horizontal tail areas (
)
4.67 m
2
Vertical tail areas (
)
2.35 m
2