{"created":"2023-06-20T15:07:59.484185+00:00","id":37374,"links":{},"metadata":{"_buckets":{"deposit":"c49120e6-6eac-408d-9772-30a35ef4bd53"},"_deposit":{"created_by":1,"id":"37374","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37374"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037374","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480415","480416","480417","480414"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Fluid flow and heat transfer in rotating curved pipes"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"377","bibliographicPageStart":"373","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":"回転曲管内の流体の流れは遠心力、コリオリ力および浮力の3種類の体積力を受ける。加熱された回転コイル管における完全層流について、類似論拠および数値的研究を通して、調べる。壁における熱的境界条件は軸方向に熱流束一定、周方向に壁温一定とする。流れと熱伝達の特徴は、これらがディーン数、プラントル数、体積力比および浮力パラメータの4つのパラメータによって支配される場合に対して、明らかにする。速度場および温度場の詳細な構造をこれらパラメータの広範囲にわたって示す。摩擦因子および平均熱伝達速度に関する計算結果も示す。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The fluid flowing in rotating heated curved pipes is subjected to three body forces: centrifugal, Coriolis and buoyant forces. Fully developed laminar flow in heated rotating coiled pipes is investigated through similarity arguments and computational studies. The thermal boundary conditions at the wall are uniform wall heat flux axially and uniform wall temperature peripherally. Flow and heat transfer characteristics are elucidated for the case when they are governed by four parameters: Dean number, Prandtl number, body force ratio and buoyancy parameter. Detailed structures of velocity and temperature fields are shown for wide range of these parameters. Computed results on the friction factor and the mean heat transfer rate are also given.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001958060","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":"航空宇宙技術研究所 角田宇宙推進技術研究センター"},{"subitem_text_value":"航空宇宙技術研究所 角田宇宙推進技術研究センター"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Kakuda Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Kakuda Research Center"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"石垣, 博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"望月, 宗和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishigaki, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mochizuki, Munekazu","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":"nalsp0041060.pdf","filesize":[{"value":"365.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0041060.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37374/files/nalsp0041060.pdf"},"version_id":"30e983aa-246a-49ce-b782-70c741e4c7a4"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"回転曲管","subitem_subject_scheme":"Other"},{"subitem_subject":"管内流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"熱伝達","subitem_subject_scheme":"Other"},{"subitem_subject":"体積力","subitem_subject_scheme":"Other"},{"subitem_subject":"遠心力","subitem_subject_scheme":"Other"},{"subitem_subject":"コリオリ力","subitem_subject_scheme":"Other"},{"subitem_subject":"遠心浮力","subitem_subject_scheme":"Other"},{"subitem_subject":"熱的境界条件","subitem_subject_scheme":"Other"},{"subitem_subject":"熱流束","subitem_subject_scheme":"Other"},{"subitem_subject":"ディーン数","subitem_subject_scheme":"Other"},{"subitem_subject":"プラントル数","subitem_subject_scheme":"Other"},{"subitem_subject":"速度場","subitem_subject_scheme":"Other"},{"subitem_subject":"温度場","subitem_subject_scheme":"Other"},{"subitem_subject":"摩擦因子","subitem_subject_scheme":"Other"},{"subitem_subject":"熱伝達速度","subitem_subject_scheme":"Other"},{"subitem_subject":"rotating curved pipe","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inpipe flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat transfer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"body force","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"centrifugal force","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Coriolis force","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"centrifugal buoyant force","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal boundary condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat flux","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Dean number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Prandtl number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"velocity field","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"temperature field","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"friction factor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat transfer rate","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":"浮力が作用する回転曲管内の流れと熱伝達","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"浮力が作用する回転曲管内の流れと熱伝達"}]},"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":"37374","relation_version_is_last":true,"title":["浮力が作用する回転曲管内の流れと熱伝達"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:20:33.735402+00:00"}