{"created":"2023-06-20T15:11:38.329026+00:00","id":41327,"links":{},"metadata":{"_buckets":{"deposit":"62c1ea56-5b04-4c59-b145-472a28c4da77"},"_deposit":{"created_by":1,"id":"41327","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41327"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041327","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489484","489483","489482","489485"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical simulation on 2D airfoil stall prediction using algebraic turbulence model"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"146","bibliographicPageStart":"141","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":"この論文では、代数型乱流のナビエ-ストークス・コードの2次元翼型失速予測への応用を示した。3種類の翼型について計算し、数値結果と実験データを比較したところ、低仰角において良い一致を示した。完全な乱流条件では失速角と最大揚力の過大評価が見られたが、この過大評価は遷移点を適切に設定することで克服できた。この論文では、剥離型の遷移点と失速角の効果について調べ、代数型乱流モデルが翼型失速をどれほど予測できるかを示した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper presents the applications of Navier-Stokes code with an algebraic turbulence to 2D (two dimensional) airfoil stall prediction. Three kinds of airfoil have been calculated and the comparison between numerical results and experimental data show good agreement in the region of low angle of attack. Overestimation of stall angle and maximum lift has observed in case of full turbulence condition, however, the overestimation can be overcome by setting transition points appropriately. In this paper the effect of transition point on separation type and stall angle is investigated and the results show the ability of algebraic turbulence model to predict airfoil stall.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635026","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":"三菱重工業"},{"subitem_text_value":"三菱重工業"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中尾, 雅弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"竹中, 啓三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakao, Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takenaka, Keizo","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":"nalsp0046026.pdf","filesize":[{"value":"2.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0046026.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41327/files/nalsp0046026.pdf"},"version_id":"caf561a7-3f9e-4331-9dc8-d04ba8c55c08"}]},"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":"代数型乱流","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ-ストークス・コード","subitem_subject_scheme":"Other"},{"subitem_subject":"失速角","subitem_subject_scheme":"Other"},{"subitem_subject":"揚力","subitem_subject_scheme":"Other"},{"subitem_subject":"失速予測","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":"2次元航空機翼","subitem_subject_scheme":"Other"},{"subitem_subject":"数値結果","subitem_subject_scheme":"Other"},{"subitem_subject":"実験データ","subitem_subject_scheme":"Other"},{"subitem_subject":"仰角","subitem_subject_scheme":"Other"},{"subitem_subject":"遷移点","subitem_subject_scheme":"Other"},{"subitem_subject":"剥離型","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":"algebraic turbulence","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stall angle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lift","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stall prediction","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":"two dimensional airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical result","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"experimental data","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angle of attack","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transition point","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"separation type","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":"代数モデルによる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":"代数モデルによる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":"41327","relation_version_is_last":true,"title":["代数モデルによる翼型失速特性シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:03:06.433908+00:00"}