机翼剖面函数及其反函数构成的保形变换与应用

On Conformal Transformation Constituted by the Function of Wing’s Section, It’s Inverse Function and Their Application

本文通过一个中间扩充复平面,最终将扩充z平面和扩充w平面联系起来,并建立起它们之间的一个等式,从而通过解这个等式得出机翼剖面函数。文中还针对扩充z平面上的一些其他区域在机翼剖面函数下保形变换到扩充z平面上的什么区域进行了讨论。

The extended complex z-plane integrated with extended complex m-plane by an intermediate extended complex plane, an equation joining these planes was established, and the function of wing＇s section was obtained by solution of the equation. The domain in an extended complex z-plane was conformally transformated from an extended complex z-plane by the function of wing＇s section is discussed.