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  1. コンテンツタイプ
  2. 紀要論文 (Departmental Bulletin Paper)
  1. 機関資料(JAXA, former ISAS, NAL, NASDA)
  2. 旧機関資料 (JAXA, former-ISAS, NAL, NASDA)
  3. 宇宙科学研究所: ISAS Report等を含む (former ISAS (The Institute of Space and Astronautical Science): Including ISAS Report etc.)
  4. Report of Aeronautical Research Institute, Tokyo Imperial University

内壓又は外壓を受ける薄肉圓筒の捩り挫屈

https://jaxa.repo.nii.ac.jp/records/35345
https://jaxa.repo.nii.ac.jp/records/35345
62137c43-ae66-4b9d-a35d-b4fc6665c198
名前 / ファイル ライセンス アクション
SA4146524.pdf SA4146524.pdf (512.2 kB)
Item type 紀要論文 / Departmental Bulletin Paper(1)
公開日 2015-03-26
タイトル
タイトル 内壓又は外壓を受ける薄肉圓筒の捩り挫屈
言語
言語 jpn
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_6501
資源タイプ departmental bulletin paper
その他のタイトル(英)
その他のタイトル On the Torsional Buckling of a Cylindrical Shell under Internal or External Pressure.
著者 吉村, 慶丸

× 吉村, 慶丸

吉村, 慶丸

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毛利, 可淳

× 毛利, 可淳

毛利, 可淳

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YOSIMURA, Yosimaru

× YOSIMURA, Yosimaru

en YOSIMURA, Yosimaru

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MORI, Yosiatu

× MORI, Yosiatu

en MORI, Yosiatu

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出版者
出版者 東京帝國大學航空研究所
出版者(英)
出版者 Aeronautical Research Institute, Tokyo Imperial University
書誌情報 東京帝國大學航空研究所報告
en : Report of Aeronautical Research Institute, Tokyo Imperial University

巻 19, 号 264, p. 347-359, 発行日 1943-07
抄録(英)
内容記述タイプ Other
内容記述 Though many papers have already been published about the problems of elastic stability of cylindrical thin shells, it appears that the analysis for the case indicated in the title has not yet been undertaken. In this paper the authors dealt with the effect of the internal or external pressure on the torsional buckling of a cylindrical shell. Firstly the infinitely long cylinder was considered for the sake of simplicity, neglecting the second order infinitesimals with regards to the small quantities α=h^2/(12a^2), [numerical formula], [numerical formula] and λ=(2πa)/l. In this case the critical stress γ_cr is given by the equation (23), expressing that the critical load as well as the circumferential wave number n after buckling, increases considerably with the internal pressure, and decreases as the external pressure increases, as will be seen in fig.1. The approximate solution for the case of the comparatively short cylinder is given in the equation (24), (25) and (26), by considering the second order terms with respect to λ. The results of the experiment carried out with the celluloid cylinders of 60cm. length with varying radius and thickness were compared with the theoretical results for the case of the short cylinder, and it was confirmed that the buckling stress ranges between 70 and 98% of the theoretical values.
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AA00387631
資料番号
内容記述タイプ Other
内容記述 資料番号: SA4146524000
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