直線翼列実験における風胴干渉と風胴壁境界層の影響について

抄録

This paper deals with the theoretical calculation of the wind tunnel interference in the cascade test on the assumption of two-dimensional potential flow and then with the influence of the wall boundary layer upon the tuning angle of flow in the cascade. Part I contains the theory of the wind tunnel wall interference upon the turning angle, and Part II the method of calculating the wall boundary layer effects upon the turning angle.