{"created":"2023-06-20T15:14:46.835779+00:00","id":44781,"links":{},"metadata":{"_buckets":{"deposit":"5e513f7e-c12d-4fde-818f-22ba26278625"},"_deposit":{"created_by":1,"id":"44781","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44781"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044781","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["471216","471212","471215","471217","471213","471214"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Static Bending Strength of Laminated CFRP Aluminum Honeycomb Sandwich Beams."}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1978-02","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"11","bibliographicVolumeNumber":"527","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-527","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper presents the results of analysis and testing conducted on the static bending strength of laminated carbon fiber reinforced plastics(CFRP) aluminum honeycomb sandwich beams. The relationship between the laminated angle of CFRP and fracture strength under pure bending was also investigated. The method of analysing the fracrure strength of laminated CFRP was as follows: the three-dimensional stress components referring to the plane including fiber were analysed, taking into account elastic failure prior to overall fracture, then comparing this with the fundamental strength corresponding to the afore-mentioned kind of fracture mechanisms of unidirectional fiber reinforced composites. Laminated CFRP aluminum honeycomb sandwich beams make use of facing laminated angles of ±45 deg/minus/plus45 deg, 90 deg/±25 deg/0 deg, 25 deg/90 deg/0 deg/-25 deg and 45 deg/90 deg/0 deg/-45 deg. In the static bending test, pieces of 5mm-thickness rubber plate and 2mm-thickness aluminum plate were attached at each loading point on the laminated CFRP aluminum honeycomb sandwich beams in order to prevent undesirable damage due to concentrated loading. It was found that fracture strength and fracture modes obtained in the CFRP aluminum honeycomb sandwich beams bending fracture test of laminated CFRP have a good correspondence with taht of analysis.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0527000","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-527","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機体第一部"},{"subitem_text_value":"航空宇宙技術研究所機体第一部"},{"subitem_text_value":"航空宇宙技術研究所機体第一部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"First Airframe Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"First Airframe Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"First Airframe Division, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"古田, 敏康"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野口, 義男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松嶋, 正道"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"FURUTA, Toshiyasu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NOGUCHI, Yoshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MATSUSHIMA, Masamichi","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":"naltr00527.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00527.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44781/files/naltr00527.pdf"},"version_id":"cbcb942b-27be-4275-bd40-226a2298d413"}]},"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":"積層CFRPハニカムサンドイッチ材の強度","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"積層CFRPハニカムサンドイッチ材の強度"}]},"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":"44781","relation_version_is_last":true,"title":["積層CFRPハニカムサンドイッチ材の強度"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:50:59.921322+00:00"}