日本航空宇宙学会誌
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
円孔,楕円孔または2円孔を有する円筒殻の応力集中
小野田 淳次郎
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ジャーナル フリー

1976 年 24 巻 272 号 p. 446-456

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The stress distribution around a circular or elliptical cutout, or two circular ones in a thin cylindrical shell is investigated under axial load, torsion or internal pressure. The analysis is based on the shallow shell theory. General solutions of the Donnell-type equations are superposed, and then the boundary condition on the free edge and the single-valued displacement condition are satisfied by a collocation procedure. The result covers wider ranges of curvature parameterβand distance between two cutouts than previous researches. Systematical investigation is done on the influence of parameter variation on stress concentration.

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© The Japan Society for Aeronautical and Space Sciences
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