{"created":"2023-06-20T14:39:49.721236+00:00","id":6638,"links":{},"metadata":{"_buckets":{"deposit":"d6883685-0381-4df6-aa28-4824dd78d2ac"},"_deposit":{"created_by":1,"id":"6638","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6638"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006638","sets":["1887:1891","9:789:1085:1366"]},"author_link":["34004","34002","34005","34003"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Two-dimensional flutter analysis using unstructured grids"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-03-25","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"213","bibliographicPageStart":"208","bibliographicVolumeNumber":"JAXA-SP-03-002","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2003論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Two-dimensional aeroelastic problems at supersonic/transonic speeds are numerically simulated. Simplified structural computations are coupled with CFD code using unstructured grids with moving boundary. In panel flutter analyses, elastic deformations are treated as a one-dimensional beam problem and the equation is solved by the finite difference method. In wing flutter analyses, a well-known bending-torsion model with two degrees of freedom is used. Both simulation results well predict flutter boundaries, namely, critical dynamic pressure or flow speeds across which flutter occurs and the accuracy of the developed method has been proved.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047427037","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-03-002","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":"塚田, はるみ"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮路, 幸二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsukada, Harumi","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":"47427037.pdf","filesize":[{"value":"785.1 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"47427037.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6638/files/47427037.pdf"},"version_id":"7fac712c-ee4a-4224-be89-4736bca6440a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"空力弾性","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"2次元モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"非構造格子","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"移動境界","subitem_subject_scheme":"Other"},{"subitem_subject":"臨界動圧","subitem_subject_scheme":"Other"},{"subitem_subject":"有限差分法","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroelasticity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unstructured grid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"moving boundary","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"critical dynamic pressure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"finite difference method","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":"非構造格子を用いた2次元フラッタ解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"非構造格子を用いた2次元フラッタ解析"}]},"item_type_id":"5","owner":"1","path":["1366","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6638","relation_version_is_last":true,"title":["非構造格子を用いた2次元フラッタ解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:51:52.770516+00:00"}