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2021
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Article
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Tab 6
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Research Article
Research on Multistage Rotor Assembly Optimization Methods for Aeroengine Based on the Genetic Algorithm
Table 6
The Monte Carlo simulation results.
Optimal solution
Maximum value (°)
Minimum value (°)
Mean value (°)
Standard deviation (°)
θz
2
180
159.62
179.88
0.2798
θz
3
180
145.91
179.89
0.7174