Abstract

A method based on the complex application of the actuator disk and finite-blade vortex theories is presented for aerodynamic design of the pusher propeller of a promising rotorcraft for vertical takeoff and landing. The software package was created that allows us to select the propeller parameters, create its 3D model and calculate aerodynamic characteristics in semi-automatic mode.

中文翻译：

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有前景的旋翼飞机推进器螺旋桨的空气动力学设计

摘要

提出了一种基于作动器盘和有限叶片涡旋理论复杂应用的方法，对有希望的垂直起降旋翼飞机的推进螺旋桨进行空气动力学设计。创建了软件包，使我们可以选择螺旋桨参数，创建其3D模型并以半自动模式计算空气动力特性。