Research Article
Coupled Lateral and Torsional Vibration of Rub-Impact Rotor during Hovering Flight
Figure 18
Orbit of disk 4 with rub-impact during hovering flight. (a) 220 rad/s. (b) 226 rad/s. (c) 236 rad/s. (d) 252 rad/s. (e) 256 rad/s. (f) 270 rad/s.
(a) |
(b) |
(c) |
(d) |
(e) |
(f) |