Research Article
Transient Response of a Simulated Aeroengine with a Fusing Structure during a Fan-Blade Out Event
Table 5
Reaction force of support bearings.
| | Position | Peak transient response (×105 N) | Amplitude of steady-state response (×105 N) |
| | 1 | 12.23 | 4.8 | | 2 | 10.58 | 4.4 | | 3 | 4.5 | 0.9 | | 4 | 3.5 | 0.6 |
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