@article{oai:jaxa.repo.nii.ac.jp:00032514,
 author = {平野, 陽一 and 小野田, 淳次郎 and 橋元, 保雄 and 相原, 賢二 and HIRANO, Yoichi and ONODA, Junjiro and HASHIMOTO, Yasuo and AIHARA, Kenji},
 issue = {4},
 journal = {東京大学宇宙航空研究所報告},
 month = {Nov},
 note = {曲げモーメント75 ton-mを受けるフレーム(円きょう)と縦通材で補強された直径2,440 mmの円筒殼の最小重量設計を行い,設計の妥当性を縮尺比1/3のモデルによる実験により確認した., A method of structural optimization is applied in designing circular cylindrical shells under bending. The cylindrical shells are stiffened both longitudinally and circumferentially. A one-third scale model of the designed cylindrical shell has been made and tested to check the validity of the design., 資料番号: SA0125803000},
 pages = {865--878},
 title = {<論文>曲げモーメントを受ける補強円筒殼の最小重量設計},
 volume = {15},
 year = {1979}
}