{"created":"2023-06-20T15:08:20.733476+00:00","id":37769,"links":{},"metadata":{"_buckets":{"deposit":"59ea89f4-b06e-4271-bcb1-efa0e2d287ea"},"_deposit":{"created_by":1,"id":"37769","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37769"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037769","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482897","482898"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Compendium of results: Aerodynamic characteristics analysis of Garabedian-Korn 75-06-12 airfoil"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"55","bibliographicPageStart":"53","bibliographicVolumeNumber":"22","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第11回航空機計算空気力学シンポジウム論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of the 11th NAL Symposium on aircraft computational aerodynamics","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 10-11 Jun. 1993 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 10-11 Jun. 1993 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航技研(NAL)特別資料SP-20に述べられた「2次元部門課題:Garabedian-Korn翼型」に対する結果報告の要約を与えた。SP-20では、提出された全ての計算結果を相互の差が分るように図にプロットした。「課題A:設計点での計算」について特に論じた。圧力分布はかなりよく一致するものの、翼弦方向の乱流境界層の特性、速度プロフィール、境界層および伴流における渦粘性係数はかなりばらつくことが判明した。そのような結果になる要因および今後に改良すべき点を論じた。本報告では結論のみを示した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A summary of the Compendium of results of two dimensional problem: Garabedian-Korn Airfoil reported in NAL SP-20 is given. In NAL SP-20 all of the submitted computation results were plotted on the respective figures to see the differences. Problem A: Design point computation was discussed significantly. Although pressure distribution gives fairly good agreement, turbulent boundary layer characteristics along chord, velocity profiles and eddy viscosity coefficient distributions in the boundary layer and wake disclosed scattered variation. The factors leading to the present results were discussed and required future improvement is discussed. In this paper only the conclusion is shown.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004171009","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-22","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":"航空宇宙技術研究所 空力性能部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"廣瀬, 直喜"}],"nameIdentifiers":[{"nameIdentifier":"482897","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Hirose, Naoki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"482898","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0022009.pdf","filesize":[{"value":"600.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0022009.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37769/files/nalsp0022009.pdf"},"version_id":"144db27b-4489-4e40-adc1-55f1d9bbd7e8"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"CFDコード性能","subitem_subject_scheme":"Other"},{"subitem_subject":"CFDコード検証","subitem_subject_scheme":"Other"},{"subitem_subject":"CFDコード比較","subitem_subject_scheme":"Other"},{"subitem_subject":"CFDワークショップ","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式数値解法","subitem_subject_scheme":"Other"},{"subitem_subject":"ワークショップ報告","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速翼型流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"ガラベディアン・コーン翼型","subitem_subject_scheme":"Other"},{"subitem_subject":"格子依存性","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層速度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"渦粘性分布","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD信頼性評価","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD code performance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD code validation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD code comparison","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD workshop","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation solution method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"workshop conpendium","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic airfoil flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Garabedian Korn airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"grid dependency","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer velocity profile","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"eddy viscosity distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD reliability assessment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Computational Fluid Dynamics","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 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