与えられた圧力分布を持つ翼型の簡易計算法

概要

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This paper deals with the problem of constructing the form of airfoil section which has given pressure distribution. The effects of angle of incidence, mean camber and thickness upon the velocity on the surface of airfoil are approximately independent of each other. This fact is utilized and from the difference of velocities on the upper and lower surfaces of the airfoil, the mean camber line and the angle of incidence are determined, while from the mean velocity, the thickness is determined. Although the labour of calculation is little, yet the result is very satisfactory. The above-mentioned method is extended to the case of wing lattice and procedure of calculation is explained.
一般社団法人日本機械学会の論文
1951-10-20