任意翼型直線翼列の特性を求める一方法(補遺)

概要

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In the previous report, a theoretical solution, in which the numerical calculation was comparatively simple due to the rapid convergency of the infinite series, was given for the flow through an arbitrary lattice, and especially the effects of the lattice arrangement and profile form were numerically clarified. In this report further researches are carried out on the inclination of the lift coefficient curve, the moment coefficient and the surface pressure distribution. These characteristics are illustrated on Clark. Y., ogival and circular are profiles arranged in various lattice conditions.
一般社団法人日本機械学会の論文