• 弯掠动叶 - 引用次数：4

  The design is caffied out for the radical and skewed-swept rotor blades, choosing reasonable main parameters and then working out the structure of rotor blades by means of aerodynamic calculation using the theory of isolated airfoils.

  本文还进行了弯掠动叶和径向动叶的设计，选取合理的参数，运用孤立翼型理论开展叶片的空气动力计算设计出叶片的构造。

  参考来源 - 弯掠动叶栅扩稳机理的研究

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