Open Access

表5

机翼优化结果对比

性能 阻力系数 翼根厚度 翼尖厚度
初始机翼 0.017 654 0.078 8 0.044 3
PSO 0.014 223 0.079 7 0.044 7
DE 0.014 161 0.079 9 0.044 8
CSA 0.014 227 0.081 1 0.044 9
RADPSO 0.014 112 0.080 0 0.044 8
EPSOBPE 0.013 979 0.079 0 0.045 4

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