The invention is in the field of configuring the shape or geometry of an aircraft airfoil. In particular, the present invention provides a method for designing an exterior geometry of an aircraft airfoil.
本发明属于配置飞行器翼型的形状或几何结构的领域。特别地,本发明提供了一种用于设计飞行器翼型的外部几何结构的方法。
Simplified method of parametric surface generation
参数表面生成的简化方法
2023-06-23
Patent
Electronic Resource
Chinese
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