{"created":"2023-06-20T15:05:19.242668+00:00","id":34617,"links":{},"metadata":{"_buckets":{"deposit":"2a5ef4c8-14e1-4f7f-af0f-055415452692"},"_deposit":{"created_by":1,"id":"34617","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"34617"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00034617","sets":["1887:1890","1896:1898:1899:1901"]},"author_link":["419962"],"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1962-07","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"2","bibliographicPageEnd":"52","bibliographicPageStart":"21","bibliographicVolumeNumber":"28","bibliographic_titles":[{"bibliographic_title":"東京大學航空研究所報告"},{"bibliographic_title":"Report/Aeronautical Research Institute, University of Tokyo","bibliographic_titleLang":"en"}]}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"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.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA2404884000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学航空研究所"}]},"item_9_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Aeronautical Research Institute, University of Tokyo"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0376-1061","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA00514444","subitem_source_identifier_type":"NCID"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"SUNAKAWA, Megumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-24"}],"displaytype":"detail","filename":"SA2404884.pdf","filesize":[{"value":"2.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA2404884.pdf","url":"https://jaxa.repo.nii.ac.jp/record/34617/files/SA2404884.pdf"},"version_id":"68f093dc-6870-4ea6-9917-743520055288"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"Deformation and Buckling of Cylindrical Shells Subjected to Heating","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Deformation and Buckling of Cylindrical Shells Subjected to Heating","subitem_title_language":"en"}]},"item_type_id":"9","owner":"1","path":["1890","1901"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"34617","relation_version_is_last":true,"title":["Deformation and Buckling of Cylindrical Shells Subjected to Heating"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T23:38:28.126728+00:00"}