进行机翼，翼身组合体的气动优化设计。
本文尝试采用气动优化设计方法进行进气道的设计。
In this dissertation, Numerical Aerodynamic Optimization method is attempted to apply in the inlet design.
压气机叶型气动优化设计目标是静压升最大和总压损失最小。
The maximization of the static pressure rise and minimization of the total pressure loss are taken as the design targets.
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