Data acquisition parameters for frequency response evaluation (modes of spindle shaft)
| Rig configuration | Modal shape (description) | Exp. frequency | FEM frequency (calibrated Model) | Absolute error | Relative error (%) |
|---|---|---|---|---|---|
| Naked rotor (No flywheel on the rotor) | Rigid tilting on transversal plane | 39 Hz | 38.6 Hz | 0.4 Hz | 1 |
| Rigid bouncing on transversal Plane | 46 Hz | 47.4 Hz | −1.4 Hz | −3 | |
| Rigid tilting on vertical plane | 84 Hz | 84.2 Hz | −0.2 Hz | −0.2 | |
| Rigid bouncing on vertical plane | 111 Hz | 111.9 Hz | −0.9 Hz | −0.8 | |
| Rotor with flywheel 4 (1, 625kg/m2) | Rigid tilting on transversal plane | 41 Hz | 38.3 Hz | 2.7 Hz | 6.6 |
| Rigid bouncing on transversal plane | 35 Hz | 36.6 Hz | −1.6 Hz | −4.6 | |
| Rigid tilting on vertical plane | 75 Hz | 77.1 Hz | −2.1 Hz | −2.8 | |
| Rigid bouncing on vertical plane | 95 Hz | 94.6 Hz | 0.4 Hz | 0.4 |
| Rig configuration | Modal shape | Exp. | FEM frequency | Absolute | Relative error (%) |
|---|---|---|---|---|---|
| Naked rotor | Rigid tilting on transversal plane | 39 Hz | 38.6 Hz | 0.4 Hz | 1 |
| Rigid bouncing on transversal Plane | 46 Hz | 47.4 Hz | −1.4 Hz | −3 | |
| Rigid tilting on vertical plane | 84 Hz | 84.2 Hz | −0.2 Hz | −0.2 | |
| Rigid bouncing on vertical plane | 111 Hz | 111.9 Hz | −0.9 Hz | −0.8 | |
| Rotor with flywheel 4 (1, 625kg/m2) | Rigid tilting on transversal plane | 41 Hz | 38.3 Hz | 2.7 Hz | 6.6 |
| Rigid bouncing on transversal plane | 35 Hz | 36.6 Hz | −1.6 Hz | −4.6 | |
| Rigid tilting on vertical plane | 75 Hz | 77.1 Hz | −2.1 Hz | −2.8 | |
| Rigid bouncing on vertical plane | 95 Hz | 94.6 Hz | 0.4 Hz | 0.4 |
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