Response orbits of the simplified rotor model 1800- 1 r 250- 1 1 1 1 1 1. FIGURE 3. Simplified rotor model for inertial nonlinearity example FIGURE 5. Root locus for linearized Vance model. 443. R = .10m m = 5 kg 1 = (1/2) mR2 a#39;o = 0.5 1 Lanbsp;...
Title | : | Rotordynamic Instability Problems in High-Performance Turbomachinery, 1988 |
Author | : | |
Publisher | : | - 1989 |
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