The drag coefficient can be reduced about 19 percent in the single design-point for wing drag design.

对于单目标机翼阻力优化设计，阻力系数减少了19%左右。

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The drag coefficient can be reduced about 19 percent in the single design-point for wing drag design.

对于单目标机翼阻力优化设计，阻力系数减少了19%左右。

youdao