@article{oai:jaxa.repo.nii.ac.jp:00031942,
 author = {平野, 陽一 and 林, 毅 and HIRANO, Yoichi and HAYASHI, Tsuyoshi},
 issue = {3},
 journal = {東京大学宇宙航空研究所報告},
 month = {Jul},
 note = {本論文で軸圧縮荷重を受ける円筒曲面板の座屈実験結果を報告する.この実験の目的は,前報告「円筒曲面板の有効幅(I)」で導いた座屈および座屈後の特性を実証することである.実験に供した曲面板の支持条件は,固定支持と考え得るものである.前報告の解析結果,(25)～(27)式を実験結果と比較する.実験値と理論曲線はよく一致している.また,座屈後の応力分布に関して興味ある現象を見出し,これに理論的説明を加えることができた., The experimental results on curved plates under axial compression are presented. The object of this experiment is to prove the formula for the buckling and post-buckling behavior of curved plates derived in the 1 st. part of this paper. The curved plates used in this experiments can be considered clamped in all edges. The analytical results obtained m the 1 st part of th s paper, Eq. (25)～(27), are compared with these experimental results. The agreement between the analytical results and the experiments is good. The interesting phenomena for the stress distribution in the post-buckling region are obtained in this experiment and the theoretical explanation is given., 資料番号: SA0125013000},
 pages = {464--475},
 title = {円筒曲面板の有効幅(II) : 実験},
 volume = {3},
 year = {1967}
}