Research on Multistage Rotor Assembly Optimization Methods for Aeroengine Based on the Genetic Algorithm

<div>The setup picture for measuring the geometric and mass parameters of the front shaft. (a) The geometric parameters are measured by a CMM. (b) The mass parameters are measured by a dynamic balancing machine.</div>

Complexity

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Figure 11

Figure 11: Research on Multistage Rotor Assembly Optimization Methods for Aeroengine Based on the Genetic Algorithm 