{"created":"2023-06-20T15:15:03.681614+00:00","id":45108,"links":{},"metadata":{"_buckets":{"deposit":"c4e02416-df45-4600-97cc-2924ae43245e"},"_deposit":{"created_by":1,"id":"45108","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45108"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045108","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["472965","472964"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical Analysis of End Effects in Symmetric Laminated Plates"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1985-01","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"11","bibliographicVolumeNumber":"850","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-850","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Stress eigenstates at the loaded end in symmetric laminated plates are discussed in this paper. The rate of attenuation of nonuniform stress distribution in composite materials is slow in comparison with that in isotropic materials. For a graphite/epoxy cross-ply laminate, for example, the characteristic length le is approximately three times that for an isotropic material. It is emphasized that the evaluation by numerical method of this decay is important in estimating the strength of composite laminated plates.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0850000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-850","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所計算センター"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Computer Center, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"奥村, 秀人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OKUMURA, Hidehito","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr00850.pdf","filesize":[{"value":"677.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00850.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45108/files/naltr00850.pdf"},"version_id":"77a95e5c-3885-452b-9410-5af55736b240"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"対称積層板における端末効果の数値解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"対称積層板における端末効果の数値解析"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"45108","relation_version_is_last":true,"title":["対称積層板における端末効果の数値解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:45:08.162040+00:00"}