{"created":"2023-06-20T15:07:32.802782+00:00","id":36909,"links":{},"metadata":{"_buckets":{"deposit":"01a0acd5-0a2a-4980-a5f2-9208552efd14"},"_deposit":{"created_by":1,"id":"36909","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36909"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036909","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["478175","478174","478171","478172","478176","478173"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"弾性モードで振動する翼周りの非定常粘性流の数値シミュレーション"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"288","bibliographicPageStart":"285","bibliographicVolumeNumber":"34","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_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所 6-7 JUN. 1996 東京 日本","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory 6-7 JUN. 1996 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"空力弾性型CFD(数値流体力学)コードを開発し、曲げモードで振動するバイオコンベックス翼断面を持つ矩形翼、および第一曲げモードで振動する高アスペクト比(YXX)翼の風洞モデルまわりの非定常遷音速流れの数値シミュレーションに適用した。第一の6つのモードを考慮してYXX翼の遷音速フラッタについても同様に数値シミュレーションを実施した。構造方程式と組合わせたナビエ・ストークス(N-S)方程式に基づくコードを用いた。N-S方程式は空力格子上のYee-Harten TVD(Total Variation Diminishing)スキームを用いて積分し、構造方程式はWilsonθ法を用いて積分した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An aeroelastic version of CFD (Computational Fluid Dynamics) code was developed and applied to numerical simulations of unsteady transonic flows around a rectangular wing with bioconvex airfoil section oscillating in bending mode and a wing tunnel model of a high aspect-ratio (YXX) wing which is also oscillating in first bending mode. A numerical simulation of transonic flutter of the YXX wing considering first six modes has been performed as well. The code is based on Navier-Stokes (N-S) equations coupled with the structural equations. The N-S equations are integrated by Yee-Harten TVD (Total Variation Diminishing) scheme on dynamic grid, while the structural side is integrated by Wilson theta method.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000685050","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-34","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":"東海大学 工学部　航空宇宙学科"},{"subitem_text_value":"東海大学 工学部　航空宇宙学科"},{"subitem_text_value":"航空宇宙技術研究所 構造力学部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokai University Department of Aeronautics and Astronautics, School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokai University Department of Aeronautics and Astronautics, School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structural Mechanics Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Kheirandish, Hamidreza"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"別府, 護朗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中道, 二郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kheirandish, Hamidreza","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Beppu, Goro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamichi, Jiro","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0034050.pdf","filesize":[{"value":"453.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0034050.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36909/files/nalsp0034050.pdf"},"version_id":"c5793a69-1df0-4592-bdc7-310b50f5a04f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"弾性モード","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常粘性流","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常遷音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"高アスペクト比","subitem_subject_scheme":"Other"},{"subitem_subject":"構造方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"振動弾性翼","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速フラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"elastic mode","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"viscous unsteady flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady transonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high aspect ratio","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structural equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"oscillating elastic wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flutter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","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":"Numerical simulation of viscous unsteady flow around wing oscillating in elastic modes","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Numerical simulation of viscous unsteady flow around wing oscillating in elastic modes","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":"36909","relation_version_is_last":true,"title":["Numerical simulation of viscous unsteady flow around wing oscillating in elastic modes"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:29:14.112331+00:00"}