{"created":"2023-06-20T15:05:18.609179+00:00","id":34606,"links":{},"metadata":{"_buckets":{"deposit":"8c00fb54-c891-4d59-9200-2f761838f2e9"},"_deposit":{"created_by":1,"id":"34606","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"34606"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00034606","sets":["1887:1890","1896:1898:1899:1901"]},"author_link":["419944","419943"],"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1960-12","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"10","bibliographicPageEnd":"213","bibliographicPageStart":"195","bibliographicVolumeNumber":"26","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 deformation and thermal stress for a rectangular plate, subjected to an arbitrary symmetrical temperature distribution, are analyzed for the case where the edges of the plate are simply supported, taking the finite deformation into account. The fundamental non-linear simultaneous partial differential equations for the thermoelastic problem are derived from the variational principle and are solved, and it is shown that, if there exists the temperature gradient through the thickness of the plate as seen in the aerodynamic heating, the plate starts to deflect at the moment of heating and does not exhibit the buckling phenomenon according to the mode of temperature distribution and the boundary conditions. Some numerical examples are given i) for the case where the temperature distribution through the thickness is specified as linear, and ii) for the case of instantaneous heating where the temperature distribution through the thickness is given in a function of time, and then some discussions on the analytical 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: SA2404851000","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":[{}]},{"creatorNames":[{"creatorName":"UEMURA, Masuji","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":"SA2404851.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA2404851.pdf","url":"https://jaxa.repo.nii.ac.jp/record/34606/files/SA2404851.pdf"},"version_id":"7d0403c3-e8d7-45f2-99f3-65fb646198ee"}]},"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 Thermal Stress in a Rectangular Plate Subjected to Aerodynamic Heating : (For the Case of Simply Supported Edges)","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Deformation and Thermal Stress in a Rectangular Plate Subjected to Aerodynamic Heating : (For the Case of Simply Supported Edges)","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":"34606","relation_version_is_last":true,"title":["Deformation and Thermal Stress in a Rectangular Plate Subjected to Aerodynamic Heating : (For the Case of Simply Supported Edges)"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T23:38:38.543387+00:00"}