{"created":"2023-07-07T08:25:59.904209+00:00","id":2000015,"links":{},"metadata":{"_buckets":{"deposit":"09359b6e-6e19-4209-bc93-c3431eb7df89"},"_deposit":{"created_by":5,"id":"2000015","owners":[5],"pid":{"revision_id":0,"type":"depid","value":"2000015"},"status":"published"},"_oai":{"id":"oai:miyazaki-u.repo.nii.ac.jp:02000015","sets":["73","73:36","73:36:330","73:36:330:496"]},"author_link":["31439"],"control_number":"2000015","item_10002_biblio_info_7":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2022-11-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"116","bibliographicPageStart":"113","bibliographicVolumeNumber":"51","bibliographic_titles":[{"bibliographic_title":"宮崎大学工学部紀要","bibliographic_titleLang":"ja"},{"bibliographic_title":"Memoirs of Faculty of Engineering, University of Miyazaki","bibliographic_titleLang":"en"}]}]},"item_10002_description_5":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"Aerodynamic characteristics of NACA 4412 airfoil were investigate by wind tunnel experiments in the region of low Reynolds number on the order of 104. In the experiment, the airfoil model made with 3D printer and twodimensional multi-fan type wind tunnel with 11 fans was used. In order to measure the micro fluid forces such as lift and drag at the low Reynolds number, 3-components force detector was applied. Airfoil surface pressure coefficients were measured by using a digital manometer from 21 pressure taps on the airfoil surface. From the experiments, it was found that as the Reynolds number decreased, the maximum lift coefficient and the maximum lift-drag ratio tended to decrease and the minimum drag coefficient tended to increase in the range of 8.0×10^3 ≤ Re ≤ 5.0×10^4.","subitem_description_language":"en","subitem_description_type":"Abstract"}]},"item_10002_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宮崎大学工学部","subitem_publisher_language":"ja"},{"subitem_publisher":"Faculty of Engineering, University of Miyazaki","subitem_publisher_language":"en"}]},"item_10002_relation_17":{"attribute_name":"関連サイト","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"宮崎大学工学部"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"https://www.miyazaki-.ac.jp/tech/research/memoirs/","subitem_relation_type_select":"URI"}}]},"item_10002_source_id_11":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA00732558","subitem_source_identifier_type":"NCID"}]},"item_10002_source_id_9":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"05404924","subitem_source_identifier_type":"ISSN"}]},"item_10002_version_type_20":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"黒木, 淳史","creatorNameLang":"ja"},{"creatorName":"クロキ, アツシ","creatorNameLang":"ja-Kana"},{"creatorName":"Kuroki, Atsushi","creatorNameLang":"en"}]},{"creatorNames":[{"creatorName":"原田, 晟覇","creatorNameLang":"ja"},{"creatorName":"ハラダ, セイラ","creatorNameLang":"ja-Kana"},{"creatorName":"Harada, Seiha","creatorNameLang":"en"}]},{"creatorAffiliations":[{"affiliationNameIdentifiers":[{"affiliationNameIdentifier":"0000000106573887","affiliationNameIdentifierScheme":"ISNI","affiliationNameIdentifierURI":"http://www.isni.org/isni/0000000106573887"}],"affiliationNames":[{"affiliationName":"宮崎大学","affiliationNameLang":"ja"},{"affiliationName":"University of Miyazaki","affiliationNameLang":"en"}]}],"creatorNames":[{"creatorName":"Shin, B.","creatorNameLang":"en"},{"creatorName":"申, 炳録","creatorNameLang":"ja"},{"creatorName":"シン, ビョンロク","creatorNameLang":"ja-Kana"},{"creatorName":"Shin, Byeongrog","creatorNameLang":"en"}],"familyNames":[{"familyName":"Shin","familyNameLang":"en"},{"familyName":"申","familyNameLang":"ja"},{"familyName":"シン","familyNameLang":"ja-Kana"},{"familyName":"Shin","familyNameLang":"en"}],"givenNames":[{"givenName":"B.","givenNameLang":"en"},{"givenName":"炳録","givenNameLang":"ja"},{"givenName":"ビョンロク","givenNameLang":"ja-Kana"},{"givenName":"Byeongrog","givenNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"31439","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2022-12-07"}],"displaytype":"detail","filename":"No51PP113-116.pdf","format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"本文","url":"https://miyazaki-u.repo.nii.ac.jp/record/2000015/files/No51PP113-116.pdf"},"version_id":"15e0dc8e-58fd-4c92-b08a-0497043490ba"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"NACA 4412 airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Low Reynolds number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Aerodynamic characteristics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Wind  tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"3-components force detector","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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"レイノルズ数 10^4 領域における NACA4412 翼型の空力特性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"レイノルズ数 10^4 領域における NACA4412 翼型の空力特性","subitem_title_language":"ja"},{"subitem_title":"Aerodynamic Characteristics of NACA4412 Airfoil in the Region of Reynolds Number 10^4","subitem_title_language":"en"}]},"item_type_id":"10002","owner":"5","path":["73","36","330","496"],"pubdate":{"attribute_name":"公開日","attribute_value":"2022-12-07"},"publish_date":"2022-12-07","publish_status":"0","recid":"2000015","relation_version_is_last":true,"title":["レイノルズ数 10^4 領域における NACA4412 翼型の空力特性"],"weko_creator_id":"5","weko_shared_id":-1},"updated":"2024-07-10T23:31:26.634205+00:00"}