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厚翼剖面的空泡特性研究
引用本文:冯丕孚.厚翼剖面的空泡特性研究[J].中国造船,1986(4).
作者姓名:冯丕孚
作者单位:中国船舶科学研究中心
摘    要:本文用奇点法解厚翼剖面局部空泡绕流问题。求解时精确考虑了空泡表面是一条流线的运动学边界条件,空泡表面压力为常数的动力学边界条件,以及水翼湿表面是一条流线的运动学边界条件,用迭代法求出了空泡表面的形状、压力分布等水动力特性,并与实验结果作了比较,得较好结果。

关 键 词:—Naval  hydrodynamics  cavitation  character  of  thick  foil  section  numerical  calcu-lation.

EXPLORATION OF CAVITATION CHARACTOR OF THICK FOIL SECTION
Feng Pifu.EXPLORATION OF CAVITATION CHARACTOR OF THICK FOIL SECTION[J].Shipbuilding of China,1986(4).
Authors:Feng Pifu
Institution:China Ship Scientific Research Center
Abstract:Partially cavitating flow passing foil section is explored using surface singularity method. The following boundary conditions, are accurately satisfied:a. kinematic boundary condition for cavity, i. e., cavity surface is a streamline;b. dynamic boundary condition for cavity, i. e., the pressure on cavity surface is constant andc. kinematic boundary condition for wetted foil section surface, i. e. wetted foil section is a streamline.An iterative procedure is used to determine hydrodynamic characteristies including cavity shape, pressure distribution and so on.Numerical calculations for a NACA16-0.15 foil section have been carried out. Agreement between calculated results and experimental data is acceptable.
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