{"created":"2023-06-20T14:39:23.978768+00:00","id":6148,"links":{},"metadata":{"_buckets":{"deposit":"119355f2-e5ba-4a4e-8cc5-4190213c7fb0"},"_deposit":{"created_by":1,"id":"6148","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6148"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006148","sets":["1887:1891","9:789:1031:1052"]},"author_link":["30779","30781","30782","30780"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"3D wing flutter analysis by bending-torsion beam model and unstructured CFD"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2006-02-28","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"99","bibliographicPageStart":"94","bibliographicVolumeNumber":"JAXA-SP-05-017","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2005論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A 3D flutter of a sweptback wing is numerically investigated by coupling inviscid flow simulations with a bending-torsion beam structure model. The beam model of a 3D wing is a natural extension of a widely used 2D 2-degree-of-freedom structure model and it considerably simplifies the structure analysis. Finite-volume unstructured CFD is used with the aim of applying various configurations in the future. The grid is dynamically deformed in accordance with the wing motion. A truss-analogy is applied to determine the new positions of interior points when the displacements of boundary points are specified. A well-known experiment using the AGARD standard aeroelastic configuration called 445.6 wing is selected for the validation. The developed methods successfully simulated the experimental flutter boundary.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049212015","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: JAXA-SP-05-017","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"横浜国立大学 大学院"},{"subitem_text_value":"横浜国立大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Yokohama National University Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Yokohama National University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"町田, 健太郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮路, 幸二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Machida, Kentaro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyaji, Koji","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":"2020-01-16"}],"displaytype":"detail","filename":"49212015.pdf","filesize":[{"value":"701.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49212015.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6148/files/49212015.pdf"},"version_id":"73fb7962-286d-46cc-9321-7e242ac4ff74"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"フラッタ解析","subitem_subject_scheme":"Other"},{"subitem_subject":"後退翼","subitem_subject_scheme":"Other"},{"subitem_subject":"翼振動","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"非構造CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"残差切除法","subitem_subject_scheme":"Other"},{"subitem_subject":"曲げ-捩り梁モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"AGARD445.6模型","subitem_subject_scheme":"Other"},{"subitem_subject":"捩り振動","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sweptback wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing oscillation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unstructured CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"residual cutting method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"bending-torsion beam model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"AGARD 445.6 model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"torsional vibration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"曲げ・捩り梁構造モデルと非構造CFDによる3次元翼フラッタ解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"曲げ・捩り梁構造モデルと非構造CFDによる3次元翼フラッタ解析"}]},"item_type_id":"5","owner":"1","path":["1052","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6148","relation_version_is_last":true,"title":["曲げ・捩り梁構造モデルと非構造CFDによる3次元翼フラッタ解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:01:18.803623+00:00"}