{"created":"2023-06-20T15:11:38.228706+00:00","id":41325,"links":{},"metadata":{"_buckets":{"deposit":"7ddd15a5-ace3-41c7-9ff5-c1c0957c7d45"},"_deposit":{"created_by":1,"id":"41325","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41325"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041325","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489474","489477","489476","489478","489479","489475"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"CDF workshop on 2D airfoil stall prediction"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"134","bibliographicPageStart":"129","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":"2次元の翼周りの流れを低速度でシミュレーションした。この研究では、定常解または準定常解を求めるために、2つの方法を試みた。マトリックスフリーのLU-SGS(Lower-Upper Symmetric Gauss Siedel)陰解法と、陰解法と陽解法を結合したハイブリッド法である。乱流モデルについては、ボールドウィン-ロマックス・モデルまたは乱流のないモデルを、圧縮型ナビエ-ストークス方程式に適用した。これらの計算結果は、実験データとよく合っていた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The flow around a 2-D (two dimensional) airfoil is simulated at a low speed. In this study two schemes are considered: the matrix-free LU-SGS (Lower-Upper Symmetric Gauss Siedel) implicit scheme and the explicit/implicit hybrid scheme to obtain steady or quasi-steady state solutions. Regarding turbulence model, either the Baldwin-Lomax model or no turbulence model is applied to the compressible Navier-Stokes equations. Results of these calculations are well compared with experimental data.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635024","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":"名古屋大学 大学院"},{"subitem_text_value":"名古屋大学 大学院工学研究科"},{"subitem_text_value":"名古屋大学 大学院工学研究科"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Nagoya University Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Nagoya University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Nagoya University Graduate School of Engineering"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"下畑, 五郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Menshov, Igor"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 佳朗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimohata, Goro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Menshov, Igor","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Yoshiaki","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":"nalsp0046024.pdf","filesize":[{"value":"498.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0046024.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41325/files/nalsp0046024.pdf"},"version_id":"f5909585-daeb-4aad-8a83-ac1f81758a01"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"翼型","subitem_subject_scheme":"Other"},{"subitem_subject":"失速特性","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析陰解法","subitem_subject_scheme":"Other"},{"subitem_subject":"ハイブリッド法","subitem_subject_scheme":"Other"},{"subitem_subject":"乱流モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮型方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ-ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"ボールドウィン-ロマックス・モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"定常解","subitem_subject_scheme":"Other"},{"subitem_subject":"準定常解","subitem_subject_scheme":"Other"},{"subitem_subject":"実験データ","subitem_subject_scheme":"Other"},{"subitem_subject":"2次元シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"airfoil type","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stall characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis implicit scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressible equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hybrid scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbulence model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Baldwin Lomax model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"steady state solution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"quasi steady state solution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"experimental data","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional 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":"ワークショップ翼型失速特性シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ワークショップ翼型失速特性シミュレーション"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41325","relation_version_is_last":true,"title":["ワークショップ翼型失速特性シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:03:10.609876+00:00"}