{"created":"2023-06-20T15:07:27.920409+00:00","id":36837,"links":{},"metadata":{"_buckets":{"deposit":"4b7e3ffb-8102-4169-8e85-fcfe13096be7"},"_deposit":{"created_by":1,"id":"36837","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36837"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036837","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["425126","425127","425125","425123","425128","425124"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"T字型CFRP補強部材の座屈後挙動の解析および実験"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"162","bibliographicPageStart":"155","bibliographicVolumeNumber":"31","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"実際の航空機構造材に一般的に使用されるT字型炭素繊維/ポリマー複合材料(CFRP)補強部材の線形座屈応力および座屈後挙動に対する数値および実験結果の比較を示した。単純な仮定にもとづいて座屈状態後の極限強度を数値的に推定した。使用したソフトウエアは市販コードNISA-2である。Rayleigh-Ritz法のような補助的な数値解析法も用いた。試験した補強部材はCF(炭素繊維)/エポキシおよびCF/PEEK(ポリエーテルエーテルケトン)製のものである。航空機構造材の大幅な軽量化には後者の材料が有力な候補であった。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A comparison between numerical and experimental results for linear buckling stress and postbuckling behavior of T-shaped Carbon Fiber Reinforced Plastics (CFRP) composite stiffeners used commonly in actual aircraft structures was described. The ultimate strength after buckled state based on rather simple assumptions was numerically estimated. The software used is the commercial level code, NISA-2. Some auxiliary numerical analysis method such as Rayleigh-Ritz method was also used. The tested stiffeners were made of CF (Carbon Fiber)/epoxy and CF/PEEK (Polyether Ether Ketone). The latter material was a potential candidate for a drastic weight reduction of aircraft structure.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000440014","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-31","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 機体部"},{"subitem_text_value":"航空宇宙技術研究所 機体部"},{"subitem_text_value":"航空宇宙技術研究所 機体部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Airframe Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Airframe Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Airframe Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"石川, 隆司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"林, 洋一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松嶋, 正道"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishikawa, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hayashi, Yoichi","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":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0031014.pdf","filesize":[{"value":"853.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0031014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36837/files/nalsp0031014.pdf"},"version_id":"6896e255-ce48-48db-b423-642aa12aa325"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"炭素繊維強化プラスチック複合材","subitem_subject_scheme":"Other"},{"subitem_subject":"CFRP","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機構造材","subitem_subject_scheme":"Other"},{"subitem_subject":"座屈後挙動","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"T字型補強部材","subitem_subject_scheme":"Other"},{"subitem_subject":"線形座屈応力","subitem_subject_scheme":"Other"},{"subitem_subject":"極限強度","subitem_subject_scheme":"Other"},{"subitem_subject":"ソフトウエア","subitem_subject_scheme":"Other"},{"subitem_subject":"NISA-2","subitem_subject_scheme":"Other"},{"subitem_subject":"Rayleigh-Ritz法","subitem_subject_scheme":"Other"},{"subitem_subject":"炭素繊維/エポキシ複合材","subitem_subject_scheme":"Other"},{"subitem_subject":"炭素繊維/ポリエーテルエーテルケトン複合材","subitem_subject_scheme":"Other"},{"subitem_subject":"軽量化","subitem_subject_scheme":"Other"},{"subitem_subject":"carbon fiber reinforced plastic composite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFRP","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"postbuckling behavior","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"T shaped stiffener","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"linear buckling stress","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ultimate strength","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"software","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NISA 2","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Rayleigh Ritz method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"carbon fiber/epoxy composite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"carbon fiber/polyether ether ketone composite","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"weight reduction","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":"Analysis and experiments of postbuckling behavior of T-shaped CFRP stiffeners","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Analysis and experiments of postbuckling behavior of T-shaped CFRP stiffeners","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"36837","relation_version_is_last":true,"title":["Analysis and experiments of postbuckling behavior of T-shaped CFRP stiffeners"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:49:26.836851+00:00"}