{"created":"2023-06-20T14:37:14.069183+00:00","id":3636,"links":{},"metadata":{"_buckets":{"deposit":"85776ab1-2a78-4146-8ba4-b48b02800133"},"_deposit":{"created_by":1,"id":"3636","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"3636"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00003636","sets":["1398:1530:1534","1543:1874:1878","1887:1891","9:789:832:1984"]},"author_link":["14602","14605","14603","14604","14607","14606"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical analysis of flow field around a NACA0012 airfoil at Re=30,000"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2016-03-08","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"84","bibliographicPageStart":"79","bibliographicVolumeNumber":"JAXA-SP-15-013","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the 47th Fluid Dynamics Conference / the 33rd Aerospace Numerical Simulation Symposium","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":"第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム (2015年7月2日-3日. 東京大学生産技術研究所), 目黒区, 東京","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":"47th Fluid Dynamics Conference /the 33rd Aerospace Numerical Simulation Symposium (July 2-3, 2015. Institute of Industrial Science , the University of Tokyo), Meguro-ku, Tokyo, Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"We calculated flow around a NACA0012 airfoil at angle of attack 7 degrees in Re=30,000 by using Open FORM to investigate a separation bubble on the upper surface side. In Re=30,000, the laminar separation was formed and the flow on the leading edge was affected by a separation bubble. The pressure distribution from the leading edge to 30% chord was constant. The flow on 50% chord reattached to a wing surface. In lower-Reynolds-number (Re=20,000), the pressure distribution on the upper surface was approximately constant from 20% chord to 80% chord. The flow on the trailing edge changed three-dimensionally. The flow field in higher-Reynolds-number (Re=40,000) was similar to the flow field in Re=30,000. We confirmed a difference in the flow on the upper surface by changing of the Reynolds number.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1630005011","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: JAXA-SP-15-013","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"日本大学"},{"subitem_text_value":"日本大学"},{"subitem_text_value":"日本大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Nihon University"},{"subitem_text_language":"en","subitem_text_value":"Nihon University"},{"subitem_text_language":"en","subitem_text_value":"Nihon University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"橋爪, 俊樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大竹, 智久"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"村松, 旦典"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashizume, Toshiki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ohtake, Tomohisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Muramatsu, Akinori","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":"2020-01-15"}],"displaytype":"detail","filename":"AA1630005011.pdf","filesize":[{"value":"2.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1630005011.pdf","url":"https://jaxa.repo.nii.ac.jp/record/3636/files/AA1630005011.pdf"},"version_id":"7c2d70e6-1fa1-4d57-b0c5-bb8ddcfb14ee"}]},"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":"RE=30,000におけるNACA0012翼まわりの流れ場の数値計算","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"RE=30,000におけるNACA0012翼まわりの流れ場の数値計算"}]},"item_type_id":"5","owner":"1","path":["1534","1878","1891","1984"],"pubdate":{"attribute_name":"公開日","attribute_value":"2016-04-21"},"publish_date":"2016-04-21","publish_status":"0","recid":"3636","relation_version_is_last":true,"title":["RE=30,000におけるNACA0012翼まわりの流れ場の数値計算"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:57:57.015340+00:00"}