In order to predict hydrodynamic characteristics a computational system is developed including determination of the pressure distribution on a wing section by use of the conformal mapping method and panel method respectively and of the flow in boundary layer according to the thin shear layer approximation ( tsl ) for navier - stokes equation approach . the wing sections of naca4412 and naca0012 are applied to test the computational system . the numerical inspection shows that the panel method with better precision and the momentum and the displacement thickness of boundary layer can be used to complete this calculation 本文分別用守屋的保角變換法和基于源匯渦分布的面元法,建立了計(jì)算槳葉表面壓力分布的數(shù)學(xué)模型;應(yīng)用納維-斯托克方程的薄層近似理論模式和有限差分?jǐn)?shù)值方法,建立了計(jì)算機(jī)翼表面邊界層內(nèi)部流動(dòng)的數(shù)學(xué)模型;應(yīng)用槳葉表面邊界層內(nèi)部粘性流動(dòng)和外部勢(shì)流流動(dòng)在邊界上的匹配算法,建立了槳葉表面二相流流動(dòng)的計(jì)算方法和相應(yīng)的計(jì)算機(jī)程序。