Shock and Vibration / 2014 / Article / Fig 17

Research Article

Rotordynamic Evaluation of Full Scale Rotor on Tilting Pad Bearings with 0.1 and 0.3 Preload

Figure 17

Effect of oil inlet temperature on the stability of rotor.
314892.fig.0017a
(a) 0.1 preload LOP
314892.fig.0017b
(b) 0.1 preload LBP
314892.fig.0017c
(c) 0.3 preload LOP
314892.fig.0017d
(d) 0.3 preload LBP