• A new method for analyzing twin-blade fixed-pitch propeller was proposed based on the theory of corrected blade foil and aerodynamic formula of 3-d wing.

    基于叶素修正理论维机翼气动系数计算公式,提出分析叶定螺旋桨方法

    youdao

  • A new method for analyzing twin-blade fixed-pitch propeller was proposed based on the theory of corrected blade foil and aerodynamic formula of 3-d wing.

    基于叶素修正理论维机翼气动系数计算公式,提出分析叶定螺旋桨方法

    youdao

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