翼型断面を有する柱体のねじり

概要

論文の詳細を見る
A method of calculating the torsional strength of the cylinders having the aerofoil sections was studied. The analysis was carried out in the rectangular co-ordinate system. As the dimentions of the aerofoils are given in rectangular co-ordinate customarily, this method is suitable for practical application. As certain examples the torsional rigidities and the shearing stress distributions of the Clark-Y series propeller section and the symmetrical section with a circular hole were oalculated.
一般社団法人日本機械学会の論文
1954-07-25