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把最优化方法与机翼的气动力求解相结合，进行跨音速机翼的气动优化设计。采用最优化方法为遗传算法，机翼的气动力由三维欧拉方程的数值解来提供。与基准机翼相比较，优化设计的机翼其气动性能有较大幅度的提高，表明遗传算法在机翼优化设计中的可行性和有效性
The optimization method is combined with the aerodynamic solution of the wing to optimize the aerodynamic design of the transonic wing. Using the optimization method as the genetic algorithm, the aerodynamic force of the wing is provided by the numerical solution of the Euler equations of three dimensions. Compared with the reference wing, the aerodynamic performance of the optimized wing has been greatly improved, which shows that the genetic algorithm is feasible and effective in wing optimization design