{"created":"2023-06-20T14:49:33.603007+00:00","id":17431,"links":{},"metadata":{"_buckets":{"deposit":"d409279b-3524-40a7-8461-9c9028929542"},"_deposit":{"created_by":1,"id":"17431","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"17431"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00017431","sets":["1543:1693:1711","1887:1891"]},"author_link":["158171","158170","158172","158173","158175","158174"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"0/90炭素-炭素複合材の硬化機構"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2002-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"12","bibliographicPageStart":"9","bibliographic_titles":[{"bibliographic_title":"宇宙輸送シンポジウム　平成13年度"},{"bibliographic_title":"Proceedings of Space Transportation Symposium FY2001","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Fracture toughness tests for cross-ply laminated carbon-carbon composites (0/90 C/Cs) were performed. These experiments aimed not only to evaluate the formation of shear bands that might be extended from the notch tips by different extension lengths but also to elucidate the interaction between 0 and 90 layers in 0/90 C/Cs. Thus, shear bands were not observed in the 0/90 C/Cs even in microscopic level, but clearly observed zigzag cracking in 0 layers, splitting in 90. This zigzag crack was yielded due to the interaction between 0 and 90 layers in these materials. The zigzag crack with partial delaminations releases a large amount of energy, which gives rise to high fracture toughness in cross-ply C/C composites.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0033392003","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Institute of Space and Astronautical Science (ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京都立大学"},{"subitem_text_value":"宇宙科学研究所"},{"subitem_text_value":"東京都立大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan University"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Metropolitan 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":"AlyHassan, Mohamed S."}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"八田, 博志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"若山, 修一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"AlyHassan, Mohamed S.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hatta, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wakayama, Shuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"硬化機構","subitem_subject_scheme":"Other"},{"subitem_subject":"炭素・炭素複合材","subitem_subject_scheme":"Other"},{"subitem_subject":"ラミネート","subitem_subject_scheme":"Other"},{"subitem_subject":"き裂","subitem_subject_scheme":"Other"},{"subitem_subject":"炭素繊維強化樹脂","subitem_subject_scheme":"Other"},{"subitem_subject":"破壊強度","subitem_subject_scheme":"Other"},{"subitem_subject":"toughening mechanism","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"carbon-carbon composite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laminate","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"crack","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"carbon fiber reinforced plastic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fracture strength","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Toughening mechanism of 0/90 carbon-carbon composites","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Toughening mechanism of 0/90 carbon-carbon composites","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1711","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"17431","relation_version_is_last":true,"title":["Toughening mechanism of 0/90 carbon-carbon composites"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:38:17.022537+00:00"}