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  2. 紀要論文 (Departmental Bulletin Paper)
  1. 機関資料(JAXA, former ISAS, NAL, NASDA)
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  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/Aeronautical Research Institute, University of Tokyo

On the Finite Deformation Mode in the Nonlinear Snap Buckling : Snap Buckling of Circular Beams Having Small Curvature under External Pressure

https://jaxa.repo.nii.ac.jp/records/34629
https://jaxa.repo.nii.ac.jp/records/34629
40f8fb0c-ca76-479b-92d4-40bbb6470d15
名前 / ファイル ライセンス アクション
SA2404920.pdf SA2404920.pdf (837.2 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 On the Finite Deformation Mode in the Nonlinear Snap Buckling : Snap Buckling of Circular Beams Having Small Curvature under External Pressure
言語 en
言語
言語 eng
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
著者 UEMURA, Masuji

× UEMURA, Masuji

en UEMURA, Masuji

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出版者
出版者 東京大学航空研究所
出版者(英)
出版者 Aeronautical Research Institute, University of Tokyo
書誌情報 東京大學航空研究所報告
en : Report/Aeronautical Research Institute, University of Tokyo

巻 29, 号 4, p. 39-53, 発行日 1964-03
抄録(英)
内容記述タイプ Other
内容記述 The nonlinear snap buckling problem of curved beams having small curvature due to external pressure, in which it is possible to obtain the exact solution, was taken up as an example to discuss the questions (1) whether or not the approximate methods usually used in the analysis of nonlinear elastic problems are proper to define the buckling load, and, (2) whether or not an unsymmetrical deflection might give a lower buckling value, as pointed out previously. The comparison of the exact solution with approximate solutions showed that the assumed deflection mode has a great influence on the buckling load. Further, the analytical result that the buckling loads obtained in the unsymmetrical mode are lower than those in symmetrical modes is found to be true only within the degree of precision of the approximate solutions themselves. The reason is that, the symmetrical deflection mode derived from the exact solution of the nonlinear equation gives the minimum buckling load. These analytical results seem to suggest the need for scrupulous attention to the assumed deflection mode in approximation method necessary for two-dimensional problems, such as problems of plates and shells.
ISSN
収録物識別子タイプ ISSN
収録物識別子 0376-1061
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AA00514444
資料番号
内容記述タイプ Other
内容記述 資料番号: SA2404920000
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