{"created":"2023-06-20T14:39:41.911355+00:00","id":6456,"links":{},"metadata":{"_buckets":{"deposit":"742a8e20-320c-417b-8f73-2b0896e0e283"},"_deposit":{"created_by":1,"id":"6456","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6456"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006456","sets":["1887:1891","9:789:1067:1073"]},"author_link":["32817","32814","32818","32816","32815","32813"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Analysis of unsteady aerodynamics of NLR-7301 wing with flap in transonic flow"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03-25","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"104","bibliographicPageStart":"99","bibliographicVolumeNumber":"JAXA-SP-04-012","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2004論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Unsteady aerodynamics of two dimensional wing of NLR-7301 which has flap was numerically investigated with Navier-Stokes code in transonic region. Shock wave motion, unsteady lift and moment coefficients are analyzed for pitch and flap motion. It is observed that the nonlinearity of unsteady aerodynamic coefficients exists in very small amplitude range for pitch and flap forced motion. Those coefficients with small amplitude show stronger nonlinearity than those with larger amplitude. There is a reattachment of boundary layer, which is generated and vanished during the forced motion at a certain condition, down stream of the shock. This enlarges the nonlinearity in smaller amplitude motion. Deviation of the first order coefficients of the unsteady aerodynamics in small amplitude range shows it effects on the flutter boundary up to 10 percent in flutter index.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0048469016","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-04-012","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":"宇宙航空研究開発機構"},{"subitem_text_value":"DLR"},{"subitem_text_value":"計算力学研究センター"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Deutsche Forschungsanstalt fur Luft- und Raumfahrt"},{"subitem_text_language":"en","subitem_text_value":"Research Center of Computational Mechanics Inc."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"齊藤, 健一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Voss, Ralph"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kheirandish, Hamidreza"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Kenichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Voss, Ralph","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kheirandish, Hamidreza","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":"48469016.pdf","filesize":[{"value":"3.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"48469016.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6456/files/48469016.pdf"},"version_id":"06f701ae-ed2c-4bf1-94cf-d76ecc341718"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"NLR7301","subitem_subject_scheme":"Other"},{"subitem_subject":"2次元翼","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機設計","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"Baldwin-Lomax乱流モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"フラップ","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層剥離","subitem_subject_scheme":"Other"},{"subitem_subject":"剥離流","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"NLR7301","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Baldwin-Lomax turbulence model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flap","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer separation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"separated flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter","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":"舵面付きNLR7301 2次元翼の遷音速非定常解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"舵面付きNLR7301 2次元翼の遷音速非定常解析"}]},"item_type_id":"5","owner":"1","path":["1073","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"6456","relation_version_is_last":true,"title":["舵面付きNLR7301 2次元翼の遷音速非定常解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:55:25.291948+00:00"}