Research Article
Response of Aeroengine with Fusing Design Suffering FBO
Table 4
Reaction force of support bearings.
| | Position | Peak value of transient response (×105 N) | Amplitude of steady response (×105 N) |
| | #1 | 12.3 | 5.0 | | #2 | 7.57 | 4.14 | | #3 | 1.65 | 0.48 | | #4 | 0.47 | 0.16 |
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