Dynamic Behavior Analysis of Intermediate Bearing-Squeeze Film Dampers-Rotor System under Constant Maneuvering Overload

Table 3

Maneuver flight parameters.

	Flight maneuvers	(g)	(m/s)	(rad/s)	(m/s)	(rad/s)
1	Hovering	10	12.12	8.08	0	0
2	Hovering	20	17.15	11.43	0	0
3	Hovering	30	21	14	0	0
4	Rolling	10	0	0	12.12	8.08
5	Rolling	20	0	0	17.15	11.43
6	Rolling	30	0	0	21	14
7	Synthetic	10	10.5	7	6.06	4.03
8	Synthetic	20	14.85	9.90	8.57	5.72
9	Synthetic	30	18.19	12.12	10.5	7