{"created":"2023-06-20T15:13:24.092654+00:00","id":43335,"links":{},"metadata":{"_buckets":{"deposit":"9bd967a8-9b53-477f-85a4-ec88b8768d51"},"_deposit":{"created_by":1,"id":"43335","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43335"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043335","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["463269","463272","463270","463271"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Unsteady Calculation of the Transonic Flow Over the ONERA-M6 Wing with a Side Wall"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1989-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"38","bibliographicPageStart":"33","bibliographicVolumeNumber":"10","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 SP-10","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The major portion of the flow field at high Reynolds number will be unsteady, so turbulent eddy viscosity models are used in simulating such high Reynolds number flow. The steady flow fields obtained by using turbulent eddy viscosity model is expected to be the time-averaged solutions. In this study, we investigated the unsteady solution of the flow over the wing with a side wall. For this purpose, we calculated the time-average of the unsteady flow field without using any turbulent eddy viscosity models. As the number of grid points gets large, the CP-curves of the time-average will become close to the results of the experiment.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0010006","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-10","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":"計算流体力学研究所"},{"subitem_text_value":"富士重工業株式会社"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"The Institute of Computational Fluid Dynamics"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"桜木, 卓也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"加茂, 圭介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakuragi, Takuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kamo, Keisuke","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":"2020-01-28"}],"displaytype":"detail","filename":"nalsp0010006.pdf","filesize":[{"value":"303.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0010006.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43335/files/nalsp0010006.pdf"},"version_id":"9dab2604-8460-4540-bcef-11b577682320"}]},"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":"側壁付きONERA-M6翼まわりの非定常計算","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"側壁付きONERA-M6翼まわりの非定常計算"}]},"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":"43335","relation_version_is_last":true,"title":["側壁付きONERA-M6翼まわりの非定常計算"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:17:09.082159+00:00"}