{"created":"2023-06-20T14:38:53.921227+00:00","id":5535,"links":{},"metadata":{"_buckets":{"deposit":"4ec9e066-1708-40d7-a912-265c2c939003"},"_deposit":{"created_by":1,"id":"5535","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5535"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005535","sets":["1887:1891","9:789:972:976"]},"author_link":["26938","26936","26933","26931","26935","26934","26937","26932"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-02-29","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"46","bibliographicPageStart":"45","bibliographicVolumeNumber":"JAXA-SP-07-026E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集　第40回"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the 40th JAXA Workshop on Investigation and Control of Boundary-Layer Transition","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Flow characteristics around aerofoil for wing in ground effect are studied experimentally in a wind tunnel. Lift and drug forces were measured directly by three-component force transducer and velocity distributions around the aerofoil were obtained by PIV (Particle Image Velocimetry). Experimental results show that lift and drag forces were consistent with the data obtained earlier qualitatively. With decreasing a ground clearance, the stagnation point moves backward and the effective angle of attack increases. For this reason, the flow rate between the aerofoil and the ground decreases, and the flow between the aerofoil and the ground is decelerated, and the pressure on the undersurface of the aerofoil increases. This is one of the causes of the wing in ground effect.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063908014","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-07-026E","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"}]},"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":"岐阜大学 工学部　機械システム工学科"},{"subitem_text_value":"岐阜大学 工学部　機械システム工学科"},{"subitem_text_value":"岐阜大学 工学部　機械システム工学科"},{"subitem_text_value":"岐阜大学 工学部　機械システム工学科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Gifu University Department of Mechanical and Systems Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Gifu University Department of Mechanical and Systems Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Gifu University Department of Mechanical and Systems Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Gifu University Department of Mechanical and Systems Engineering, Faculty of Engineering"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"菊地, 聡"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小里, 泰章"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"今尾, 茂樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"三井, 浩之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kikuchi, Satoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kozato, Yasuaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Imao, Shigeki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mitsui, Hiroyuki","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":"2020-01-16"}],"displaytype":"detail","filename":"63908014.pdf","filesize":[{"value":"396.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63908014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5535/files/63908014.pdf"},"version_id":"872e4e01-5c40-4b8d-8c58-a85b326bb312"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"翼型","subitem_subject_scheme":"Other"},{"subitem_subject":"速度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"揚抗比","subitem_subject_scheme":"Other"},{"subitem_subject":"地面効果","subitem_subject_scheme":"Other"},{"subitem_subject":"迎角","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"流体力","subitem_subject_scheme":"Other"},{"subitem_subject":"翼端渦","subitem_subject_scheme":"Other"},{"subitem_subject":"前縁","subitem_subject_scheme":"Other"},{"subitem_subject":"よどみ点","subitem_subject_scheme":"Other"},{"subitem_subject":"最低地上高","subitem_subject_scheme":"Other"},{"subitem_subject":"airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"velocity distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lift drag ratio","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ground effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angle of attack","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic force","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing tip vortice","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"leading edge","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stagnation point","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ground clearance","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"The velocity distribution around aerofoil for wing in ground effect","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"The velocity distribution around aerofoil for wing in ground effect","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["976","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5535","relation_version_is_last":true,"title":["The velocity distribution around aerofoil for wing in ground effect"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:12:38.264963+00:00"}