Shock and Vibration / 2014 / Article / Fig 18

Research Article

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

Figure 18

Effect of oil inlet temperature on the stability of rotor.
314892.fig.0018a
(a) 0.1 preload LOP
314892.fig.0018b
(b) 0.1 preload LBP
314892.fig.0018c
(c) 0.3 preload LOP
314892.fig.0018d
(d) 0.3 preload LBP