{"created":"2023-06-20T15:11:38.526637+00:00","id":41331,"links":{},"metadata":{"_buckets":{"deposit":"da3ca75d-8cdd-4e41-8bc1-a41f2124bc9d"},"_deposit":{"created_by":1,"id":"41331","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41331"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041331","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489514","489505","489507","489509","489506","489513","489510","489511","489512","489504","489508","489515"],"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 2D airfoil stall by UPACS: CFD Workshop on 2D airfoil stall predict"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"168","bibliographicPageStart":"163","bibliographicVolumeNumber":"46","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_3_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 7-9 Jun. 2000 東京 日本","subitem_description_type":"Other"}]},"item_3_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 7-9 Jun. 2000 Tokyo Japan","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"3種類の2次元翼の静的失速現象について数値的に調べた。UPACS(航空宇宙計算シミュレーション統一基準)とスパラート-アルマラス乱流モデルを用いた。これは、風洞実験とCFD(計算流体力学)の結果を比べると、NACA633-018、NACA631-012の翼型失速特性を性能良く予測できた。NACA64A-006については、CFDは完全乱流での層剥離と乱流の再付着をシミュレートできなかった。しかし、あらかじめ与えた人工的な遷移点を設けると、数値的手法は層剥離泡と乱流の再付着をとらえることができた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Static stall phenomena of three kinds of 2D (two dimensional) airfoil, are numerically investigated. UPACS (Unified Platform for Aerospace Computational Simulation) is used with Spalart-Allmaras turbulence model showing good performance to predict airfoil stall characteristics for NACA633-018 and NACA631-012, comparing CFD (Computational Fluid Dynamics) results with wind tunnel testing data. As for NACA64A-006, CFD cannot simulate a laminar separation and turbulent reattachment assuming a fully turbulent flow. However, a numerical method with an artificial transition point which is apriori given, can capture laminar separation bubble and turbulent reattachment.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635030","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-46","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 UPACSチーム"},{"subitem_text_value":"航空宇宙技術研究所 UPACSチーム"},{"subitem_text_value":"航空宇宙技術研究所 UPACSチーム"},{"subitem_text_value":"航空宇宙技術研究所 UPACSチーム"},{"subitem_text_value":"航空宇宙技術研究所 UPACSチーム"},{"subitem_text_value":"航空宇宙技術研究所 UPACSチーム"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory UPACS Team"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory UPACS Team"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory UPACS Team"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory UPACS Team"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory UPACS Team"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory UPACS Team"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"高木, 亮治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 一臣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"榎本, 俊治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山崎, 裕之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山根, 敬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩宮, 敏幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takaki, Ryoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Kazuomi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Enomoto, Shunji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamazaki, Hiroyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamane, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwamiya, Toshiyuki","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":"nalsp0046030.pdf","filesize":[{"value":"783.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0046030.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41331/files/nalsp0046030.pdf"},"version_id":"a476b637-c923-4751-aac7-4afbd43561a7"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"2次元翼","subitem_subject_scheme":"Other"},{"subitem_subject":"静的失速現象","subitem_subject_scheme":"Other"},{"subitem_subject":"UPACS","subitem_subject_scheme":"Other"},{"subitem_subject":"スパラート-アルマラス乱流","subitem_subject_scheme":"Other"},{"subitem_subject":"失速特性","subitem_subject_scheme":"Other"},{"subitem_subject":"層剥離","subitem_subject_scheme":"Other"},{"subitem_subject":"乱流再付着","subitem_subject_scheme":"Other"},{"subitem_subject":"最大揚力","subitem_subject_scheme":"Other"},{"subitem_subject":"剥離泡","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"乱流","subitem_subject_scheme":"Other"},{"subitem_subject":"数値計算法","subitem_subject_scheme":"Other"},{"subitem_subject":"人為的遷移点","subitem_subject_scheme":"Other"},{"subitem_subject":"航空宇宙計算シミュレーション統一基準","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"static stall phenomenon","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"UPACS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Spalart Allmaras turbulence","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stall characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laminar separation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbulent reattachment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"peak lift","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"separation bubble","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbulent flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"artificial transition point","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Unified Platform for Aerospace Computational 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 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