{"created":"2023-06-20T14:35:44.064149+00:00","id":2009,"links":{},"metadata":{"_buckets":{"deposit":"4dfee70b-1157-4bcb-93f0-901ee087cc3d"},"_deposit":{"created_by":1,"id":"2009","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2009"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002009","sets":["1887:1893","9:10:87:93"]},"author_link":["2271","2275","2276","2281","2284","2283","2273","2270","2274","2279","2280","2272","2282","2285","2278","2277"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Modification of CFD surface mesh based on model deformation measurement"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-03-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"18","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RR-12-004","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"風洞試験で計測した模型変形データを用いて，Computational Fluid Dynamics（CFD）表面格子を修正する方法を検討する．JAXA ではマーカーを使ったステレオ写真法により風試模型の模型変形量を計測しており，計測したマーカー座標値を使うことで主翼の変形則を同定し，変形後の形状を定義することができる．本報告では，計測したマーカー座標値を使って変形後の形状を同定し，CFD の表面格子が通風時の風試模型形状と一致するように修正する方法を検討する．ここでは三種類の変形手法を検討する．そして，実際に模型の変形量を計測したDLR-F6FX2B モデルに対して本手法を適用し，変形モデルの検証をおこなう．また，変形前後の形状に対して Reynolds-averaged Navier-Stokes（RANS）解析を実施することで，変形を考慮していない場合と考慮した場合とで空力特性にどの程度影響を及ぼすかを検討する．","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Modification approach of a computational fluid dynamics（CFD） surface mesh are examined using measurement data of wind tunnel model deformation. Model deformation measurements (MDM) were successfully made at Japan aerospace exploration agency (JAXA) using stereo photogrammetry with markers. The model's deformation was then approximated using a deformation law which is identified by a few parameters with markers attached on the wind tunnel model. In this paper, the approach is used to rearrange the CFD surface mesh of a CFD model to conform its configuration with that of the wind tunnel test model. We duplicate the deformed configuration of the wind tunnel model using three deformation laws and examine the resulting CFD models. A high-fidelity RANS simulation of the DLR-F6 FX2B wind tunnel model is then performed considering the static deformation of the model and the effct of model deformation on the aerodynamic characteristics are also exp\"\" lored by performing the CFD simulation for the deformed configuration as well as the original (non-deformed) configuration.","subitem_description_type":"Other"}]},"item_3_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_3_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0061957000","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: JAXA-RR-12-004","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1113","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":"AA1192675X","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構研究開発本部流体グループ (JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部流体グループ (JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部数値解析グループ(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部数値解析グループ(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部風洞技術開発センター(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部風洞技術開発センター(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構研究開発本部流体グループ (JAXA)"},{"subitem_text_value":"菱友システムズ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fluid Dynamics Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Fluid Dynamics Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Numerical Analysis Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Numerical Analysis Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Fluid Dynamics Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Fluid Dynamics Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Fluid Dynamics Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Ryoyu Systems Co. Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"保江, かな子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"口石, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋本, 敦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"村上, 桂一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"加藤, 裕之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中北, 和之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡辺, 重哉"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"菱田, 学"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yasue, Kanako","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kuchiishi, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashimoto, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Murakami, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kato, Hiroyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakakita, Kazuyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Shigeya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hishida, Manabu","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":"2020-01-15"}],"displaytype":"detail","filename":"61957000.pdf","filesize":[{"value":"2.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"61957000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2009/files/61957000.pdf"},"version_id":"6c2595b3-1732-4e41-8993-535691d3a41c"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"static aeroelasticity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind-tunnel model deformation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flow simulation","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"模型変形計測データを反映したCFD表面格子修正法の開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"模型変形計測データを反映したCFD表面格子修正法の開発"}]},"item_type_id":"3","owner":"1","path":["93","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2009","relation_version_is_last":true,"title":["模型変形計測データを反映したCFD表面格子修正法の開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:30:27.203308+00:00"}