翼型のキャビテーション性能について

概要

論文の詳細を見る
To solve two-dimensional flow around an aerofoil, conformal representation which transforms the given aerofoil into a circle, is usually applied. The constants in the mapping function are determined by the profile-form, and in this paper, a method of obtaining these constants from the ordinary camber values at points of 0,1.25,2.5,……, 100% of the chord is explained. From the numerical examples the starting points of cavitation on the surface of aerofoil are determined and compared with experimental results.
一般社団法人日本機械学会の論文
1951-10-20