{"created":"2023-06-20T15:07:59.679981+00:00","id":37378,"links":{},"metadata":{"_buckets":{"deposit":"2ce5e05f-752c-4b14-8d38-71cb9dac7218"},"_deposit":{"created_by":1,"id":"37378","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37378"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037378","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480433","480432","480437","480430","480435","480431","480434","480436"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Large-scale numerical simulation of flow over an airfoil"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"402","bibliographicPageStart":"397","bibliographicVolumeNumber":"41","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_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 24-26 Jun. 1998 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 24-26 Jun. 1998 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"最近、コンピュータ性能の発達により乱流の大型数値計算が可能となった。本報では、実際的な直接数値計算(DNS)および大規模渦シミュレーション(LES)技術を開発するために、後退角のないNACA0012翼のまわりの流れについて行った数値解析の研究を報告する。レイノルズ数Reは、一様流入速度とコード長さに基づいて、2.0×10(exp 6)にした。計算はNALの高処理性能並列計算機NWT(数値風洞)で現在行っている。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Recently, the development of computer power has enabled to make large scale numerical simulation for turbulent flows. In this paper, studies on the simulation of flow around the NACA0012 airfoil without sweep are reported in order to develop the practical DNS (Direct Numerical Simulation) and LES (Large Eddy Simulation) technologies. The Reynolds number Re, based on the uniform inflow velocity and the chord length, is set to be 2.0 x 10(exp 6). Computations are now under going with the high performance parallel supercomputer NWT (Numerical Wind Tunnel) at NAL.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001958064","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-41","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":"東京理科大学 大学院理工学研究科"},{"subitem_text_value":"富山大学 工学部　機械知能システム工学科"},{"subitem_text_value":"東京理科大学 理工学部　機械工学科"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Science University of Tokyo Graduate School of Science and Technology"},{"subitem_text_language":"en","subitem_text_value":"Toyama University Dept. of Mechanical and Intellectual Systems Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Science University of Tokyo Department of Mechanical Engineering, Faculty of Science and Technology"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"飯田, 博将"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐竹, 信一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"河村, 洋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松尾, 裕一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iida, Hiromasa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Satake, Shinichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawamura, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuo, Yuichi","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":"nalsp0041064.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0041064.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37378/files/nalsp0041064.pdf"},"version_id":"b743ef1a-dd79-4de3-bf89-a7847e94fe19"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"翼周りの流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"大規模数値計算","subitem_subject_scheme":"Other"},{"subitem_subject":"直接数値計算","subitem_subject_scheme":"Other"},{"subitem_subject":"DNS","subitem_subject_scheme":"Other"},{"subitem_subject":"大規模渦シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"LES","subitem_subject_scheme":"Other"},{"subitem_subject":"乱流","subitem_subject_scheme":"Other"},{"subitem_subject":"レイノルズ数","subitem_subject_scheme":"Other"},{"subitem_subject":"並列計算機","subitem_subject_scheme":"Other"},{"subitem_subject":"NWT","subitem_subject_scheme":"Other"},{"subitem_subject":"数値風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"flow around a wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"large scale numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"direct numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"DNS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"large eddy simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"LES","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbulent flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Reynolds number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"parallel supercomputer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NWT","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical wind tunnel","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 paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"翼まわりの大規模数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"翼まわりの大規模数値シミュレーション"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37378","relation_version_is_last":true,"title":["翼まわりの大規模数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:20:25.893824+00:00"}