{"created":"2023-06-20T15:08:18.725512+00:00","id":37728,"links":{},"metadata":{"_buckets":{"deposit":"c4cb96f8-cd60-4678-b557-6c16c7a62b5d"},"_deposit":{"created_by":1,"id":"37728","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37728"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037728","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482698","482699","482701","482700"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Development of buoyancy affected laminar flow in a heated pipe"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"233","bibliographicPageStart":"229","bibliographicVolumeNumber":"19","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第10回航空機計算空気力学シンポジウム論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of the NAL symposium on aircraft computational aerodynamics","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 10-12 Jun. 1992 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 10-12 Jun. 1992 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"水平に置かれた管の中の発達する層流流れおよび熱伝達に対する浮力の効果を数値的に調べた。熱的境界条件は、軸方向には熱流束一定、周方向には壁温一定とした。摩擦係数、流れのパターンおよびヌッセルト数についての結果を論じた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The effects of buoyancy on developing laminar flow and heat transfer in a horizontal pipe are analyzed numerically. Thermal boundary conditions are axially constant wall heat flux and peripherally constant wall temperature. The results on friction factor, flow pattern, Nusselt number are discussed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004168042","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-19","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 角田支所"},{"subitem_text_value":"航空宇宙技術研究所 角田支所"}]},"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":"望月, 宗和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石垣, 博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mochizuki, Munekazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishigaki, Hiroshi","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":"nalsp0019042.pdf","filesize":[{"value":"418.2 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flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heated pipe flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"duct wall friction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"duct heat transfer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"buoyancy effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"secondary flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Prandtl number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Nusselt number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"internal flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation solution","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 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