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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/Aeronautical Research Institute, University of Tokyo

Deformation and Buckling of Cylindrical Shells Subjected to Heating

https://jaxa.repo.nii.ac.jp/records/34617
https://jaxa.repo.nii.ac.jp/records/34617
26285e6f-5afc-4226-90a9-b138bf51c5ff
名前 / ファイル ライセンス アクション
SA2404884.pdf SA2404884.pdf (2.2 MB)
Item type 紀要論文 / Departmental Bulletin Paper(1)
公開日 2015-03-26
タイトル
タイトル Deformation and Buckling of Cylindrical Shells Subjected to Heating
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 SUNAKAWA, Megumi

× SUNAKAWA, Megumi

en SUNAKAWA, Megumi

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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 28, 号 2, p. 21-52, 発行日 1962-07
抄録(英)
内容記述タイプ Other
内容記述 The problems of thermal deformation and bucking of cylindrical shells arise in connection with air-frame bodies subjected to the aerodynamic heating at supersonic speeds and with combustion chambers and exhaust pipes exposed to extremely hot gases. The authors analyzed previously the thermal deformations of flat plates and pointed out that it was impossible to disregard the effect of temperature gradient through the thickness on their deformations depending on the temperature distribution and the boundary conditions. In this paper, the deformation and buckling of cylindrical shells subjected to heating are analyzed. Taking the finite deformation into account, the fundamental non-linear simultaneous partial differential equations for the thermoelastic problems of a cylindrical shell, including also the terms concerning the normal pressure as well as the effect of temperature gradient through the thickness, are derived from the variational principle and are analyzed for the following three extreme cases, that is, for the cases where i) the cylindrical shell, subjected to heating and normal pressure, is free from the constraints upon the thermal expansion and the axial displacement, but restrained laterally against the pressure at the edges, ii) the cylindrical shell is unrestrained longitudinally but fully restrained laterally at the edges, and iii) the cylindrical shell is clamped completely at the edges, and then some discussions on analytical and numerical results are given.
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: SA2404884000
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