{"created":"2023-06-20T15:13:23.278565+00:00","id":43322,"links":{},"metadata":{"_buckets":{"deposit":"6b6c7ed7-8c2f-4827-8f69-ed64c30b0eb6"},"_deposit":{"created_by":1,"id":"43322","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43322"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043322","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["463199","463200"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical Simulation of Unsteady Aerodynamics Around an Oscillating Wing in Elastic Modes"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1988-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"214","bibliographicPageStart":"205","bibliographicVolumeNumber":"9","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 SP-9","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Unsteady Navier-Stokes calculations around arifoil/wing are demonstrated. 2D transonic flutter simulations are performed about NACA 64A010 airfoil using not only a diagonal form of Beam-Warming scheme but also a non-diagonal one. The effects of time accuracy of the algorithms on the flutter boundaries are checked by comparing two results. 3D unsteady computations around an oscillating wing in elastic motions are also carried out and obtained results are compared with experimental data. It is found that the diagonal form of Beam-Warming scheme is efficient to predict the flutter boundaries of airfoils in case where the flow is not separated. It is also demonstrated that the present 3D code gives results in agreements with experimental data and it can be used for 3D flutter simulation program in a similar manner to 2D case.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0009031","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 SP-9","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":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_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_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所構造力学部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中道, 二郎"}],"nameIdentifiers":[{"nameIdentifier":"463199","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Nakamichi, Jiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"463200","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":"2020-01-28"}],"displaytype":"detail","filename":"nalsp0009031.pdf","filesize":[{"value":"665.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0009031.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43322/files/nalsp0009031.pdf"},"version_id":"00532892-ca67-4da7-a729-4a1e06161148"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"弾性モードを考慮した3次元振動翼まわりの非定常空気力の数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"弾性モードを考慮した3次元振動翼まわりの非定常空気力の数値シミュレーション"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43322","relation_version_is_last":true,"title":["弾性モードを考慮した3次元振動翼まわりの非定常空気力の数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:17:26.859575+00:00"}