{"created":"2023-06-20T15:10:44.539024+00:00","id":40315,"links":{},"metadata":{"_buckets":{"deposit":"54de9062-2ea5-4435-a1b4-f11b72839a0d"},"_deposit":{"created_by":1,"id":"40315","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40315"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040315","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["447309","447313","447307","447314","447306","447308","447315","447310","447312","447311"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"ファイバ/メタル積層材料GLARE3-5/4の疲労き裂進展特性"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"13","bibliographicPageStart":"1","bibliographicVolumeNumber":"1368T","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本研究の目的は、ファイバメタル積層材料GLARE3-5/4における疲労き裂進展特性を調べるとともに、ファイバメタル積層材料におけるき裂進展を解析する方法の有効性について調べることである。GLARE3-5/4は5枚のアルミニウム合金薄板とガラス/エポキシ4層からなる。中央部に切欠きを有する試験片に対して一定振幅荷重下の疲労試験を行い、き列長さをDCポテンシャルドロップ法により測定した。また、アルミニウム合金シートと繊維・接着層との層間剥離の大きさは、き裂周りを超音波C-スキャンにより撮影した写真から計測した。試験結果は、GLARE3-5/4における疲労き裂進展の特徴を明らかにした。また試験結果に基づき、ファイバメタル積層材料におけるき裂進展を解析する2種類の方法について、その有効性を検討した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The objective of this study is to investigate the properties of fatigue crack growth in GLARE3-5/4 fiber/metal laminate and the validity of methods for analyzing the fatigue crack growth of fiber/metal laminates. GLARE3-5/4 consists of five thin sheets of 2024-T3 aluminum alloy and four layers of (0/90) glass/epoxy. Centrally notched specimens were fatigue tested under constant amplitude loading and crack length was measured using the DC potential drop method. The size of the delamination produced between aluminum alloy sheets and fiber adhesive layers was measured from ultrasonic C-scan pictures taken around the fatigue crack. The test results indicated the features of fatigue crack growth in GLARE3-5/4. The validity of two methods for analyzing the fatigue crack growth of fiber/metal laminates is discussed based on the test results.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001675000","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-1368T","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"},{"subitem_text_value":"電気通信大学"},{"subitem_text_value":"松下通信工業"},{"subitem_text_value":"航空宇宙技術研究所 構造研究部"},{"subitem_text_value":"航空宇宙技術研究所 構造研究部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"University of Electro-Communications"},{"subitem_text_language":"en","subitem_text_value":"Matsushita Communication Industrial Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structures Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structures Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"高松, 徹"}],"nameIdentifiers":[{"nameIdentifier":"447306","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"松村, 隆"}],"nameIdentifiers":[{"nameIdentifier":"447307","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"小倉, 紀男"}],"nameIdentifiers":[{"nameIdentifier":"447308","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"下河, 利行"}],"nameIdentifiers":[{"nameIdentifier":"447309","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"角田, 義秋"}],"nameIdentifiers":[{"nameIdentifier":"447310","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Takamatsu, Toru","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"447311","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Matsumura, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"447312","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Ogura, Norio","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"447313","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Shimokawa, Toshiyuki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"447314","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Kakuta, Yoshiaki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"447315","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-27"}],"displaytype":"detail","filename":"naltr0001368t.pdf","filesize":[{"value":"576.5 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001368t.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40315/files/naltr0001368t.pdf"},"version_id":"6ef97e43-720a-49e6-be5c-67d50fdea84b"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"ファイバメタル積層材料","subitem_subject_scheme":"Other"},{"subitem_subject":"ガラス繊維","subitem_subject_scheme":"Other"},{"subitem_subject":"アルミニウム合金","subitem_subject_scheme":"Other"},{"subitem_subject":"疲労き裂伝ぱ","subitem_subject_scheme":"Other"},{"subitem_subject":"GLARE","subitem_subject_scheme":"Other"},{"subitem_subject":"疲労き裂進展","subitem_subject_scheme":"Other"},{"subitem_subject":"ファイバブリッジング","subitem_subject_scheme":"Other"},{"subitem_subject":"剥離","subitem_subject_scheme":"Other"},{"subitem_subject":"最大応力依存性","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機構造材","subitem_subject_scheme":"Other"},{"subitem_subject":"fiber metal laminate","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"glass fiber","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aluminum alloy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fatigue crack propagation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"GLARE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fatigue crack growth","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fiber bridging","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"delamination","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"maximum stress dependence","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft structure material","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"Fatigue crack growth properties of a GLARE3-5/4 fiber/metal laminate","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Fatigue crack growth properties of a GLARE3-5/4 fiber/metal laminate","subitem_title_language":"en"}]},"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":"40315","relation_version_is_last":true,"title":["Fatigue crack growth properties of a GLARE3-5/4 fiber/metal laminate"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:15:33.391684+00:00"}