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  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/Aeronautical Research Institute, University of Tokyo

On the Solution of Nonlinear Snap Buckling by the Progressive Approximation Method : Snap Buckling of Spherical Shells under Uniform External Pressure

https://jaxa.repo.nii.ac.jp/records/34630
https://jaxa.repo.nii.ac.jp/records/34630
22089b6a-22ac-464c-8839-454637c824d6
名前 / ファイル ライセンス アクション
SA2404923.pdf SA2404923.pdf (624.1 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 Solution of Nonlinear Snap Buckling by the Progressive Approximation Method : Snap Buckling of Spherical Shells under Uniform 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 5, p. 55-65, 発行日 1964-03
抄録(英)
内容記述タイプ Other
内容記述 A set of nonlinear differential equations based on the finite deformation theory in the two-dimensional shells has been solved by assuming a specified deflection mode because of the difficulty to obtain their exact solution ; however, the particular deflection mode assumed has a great effect on the buckling load, giving considerably higher theoretical values than experimental values, as noted in he previous paper. From the above circumstances, the progressive approximation method was applied to the snap bucking problem under uniform pressure of a shallow spherical shell segment having small value of α=αβ^2/t(a ; radius, t ; thickness, 2β ; angle of opening) and a more precise and reasonable solution could be obtained by means of a comparatively simple mathematical treatment. That is, much lower initial buckling loads were obtained with the deflection mode which varied reasonably with the variations of load and deflection, verifying the appropriateness of this method.
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: SA2404923000
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