{"created":"2023-06-20T14:54:12.629458+00:00","id":22493,"links":{},"metadata":{"_buckets":{"deposit":"fd42037f-ad6e-4b56-9462-f7f20dd3c992"},"_deposit":{"created_by":1,"id":"22493","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"22493"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00022493","sets":["1887:1888"]},"author_link":["210919","210921","210926","210918","210920","210924","210925","210923","210927","210922"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Out-of-Plane Tensile Modulus of CFRP Laminates by 3-Point Bending Test"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-09-15","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"5","bibliographicPageEnd":"192","bibliographicPageStart":"184","bibliographicVolumeNumber":"39","bibliographic_titles":[{"bibliographic_title":"日本複合材料学会誌"},{"bibliographic_title":"Journal of the Japan Society for Composite Materials","bibliographic_titleLang":"en"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"To propose a test method for the out-of plane tensile modulus of laminated carbon fiber-reinforced plastics, 3-point bending tests using a laminated CGRP with the span direction coinciding with out-of-plane (through-the-thickness) direction were performed. It was demonstrated that the apparent bending modulus depends on the length of span to thickness ratio (L/t) and the tensile modulus E to shear modulus G ratio (E/G). Sensitivity analyses were performed to select the length of span to thickness ratio in order to evaluate the bending modulus near material modulus. Consequently, it is predicted that the bending modulus performed with the L/t >25 bending specimen is equivalent to tensile modulus, if the apparent bending modulus were evaluated from 1 to 15GPa, while modified equations for the out-of-plane modulus of QI-CFRP laminates obtained by three-dimensional laminate theory were also derived. This modification took stress condition in consideration of the small in-plane size like bending specimens into account. Moreover, it is demonstrated that apparent bending moduli were evaluated between upper and lower-bound solutions. The upper-bound solution is an out-of-plane modulus based on existing three-dimensional laminate theory, and the other is modified out-of-plane modulus.","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA1420046000","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本複合材料学会"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Japan Society for Composite Materials"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.6089/jscm.39.184"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.6089/jscm.39.184","subitem_relation_type_select":"DOI"}}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0385-2563","subitem_source_identifier_type":"ISSN"}]},"item_7_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00196748","subitem_source_identifier_type":"NCID"}]},"item_7_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構航空本部(JAXA)"},{"subitem_text_value":"東京大学"},{"subitem_text_value":"宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)"},{"subitem_text_value":"宇宙航空研究開発機構航空本部(JAXA)"},{"subitem_text_value":"名古屋大学"}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"The University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"},{"subitem_text_language":"en","subitem_text_value":"Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Nagoya University"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"原, 栄一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"横関, 智弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"八田, 博志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩堀, 豊"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石川, 隆司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hara, Eiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yokozeki, Tomohiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hatta, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwahori, Yutaka","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishikawa, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Out-of-plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mechanical properties","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Test method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Bending test","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"3点曲げ試験による積層CFRPの面外方向引張弾性率","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"3点曲げ試験による積層CFRPの面外方向引張弾性率"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"22493","relation_version_is_last":true,"title":["3点曲げ試験による積層CFRPの面外方向引張弾性率"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:20:13.651418+00:00"}