{"created":"2023-05-15T12:05:36.124604+00:00","id":10285,"links":{},"metadata":{"_buckets":{"deposit":"08ab09c5-72f2-4433-87c8-0b4bcd814ef1"},"_deposit":{"created_by":3,"id":"10285","owners":[3],"pid":{"revision_id":0,"type":"depid","value":"10285"},"status":"published"},"_oai":{"id":"oai:iwate-u.repo.nii.ac.jp:00010285","sets":["1515:1519"]},"author_link":["63744","63738","63737","63736","63742","63743","63739","63741","63735","63745","63740","63734"],"item_16_alternative_title_23":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"Studies on High-Lift LP Turbine Airfoils of Aero Engines (Understanding of Time-Averaged Behaviour of Separated Boundary Layer under the Influence of Incoming Wakes)"}]},"item_16_biblio_info_7":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2008-01-01","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"741","bibliographicPageEnd":"1048","bibliographicPageStart":"1040","bibliographicVolumeNumber":"74","bibliographic_titles":[{"bibliographic_title":"日本機械学会論文集B編"}]}]},"item_16_date_6":{"attribute_name":"登録日","attribute_value_mlt":[{"subitem_date_issued_datetime":"2013-12-16"}]},"item_16_description_12":{"attribute_name":"Abstract","attribute_value_mlt":[{"subitem_description":"This paper details experimental studies on the flow field around a low-pressure linear turbine\ncascade whose solidity is changeable. Highly loaded low-pressure turbine (LPT) blades or ultrahigh\nlift airfoils are one of the key paths to successful future aero-engines, however those blades are\nusually accompanied with separation bubble, eventually leading to the increase in aero dynamic loss.\nThe purpose of this study is to clarify the effect of incoming wakes upon the aerodynamic loss of the\nrotor blade cascade, through the measurements of wake-affected boundary layers upon including\nseparation bubble for low Reynolds number conditions and/or low solidity conditions. Cylindrical\nbars on the timing belts work as wake generator to emulate upstream stator wakes that impact the\nrotor blade. Hot-wire probe measurement is conducted over the blade suction surface to understand\nto what extent and how the incoming wakes affect the boundary layers containing separation bubble.\nIn particular, from the viewpoint of providing database for blade designing, this paper focuses on\ntime-averaged characteristics of the separated boundary layer influenced by the wake passing.","subitem_description_type":"Other"}]},"item_16_full_name_3":{"attribute_name":"著者別名","attribute_value_mlt":[{"nameIdentifiers":[{"nameIdentifier":"63740","nameIdentifierScheme":"WEKO"}],"names":[{"name":"FUNAZAKI, Ken-ichi"}]},{"nameIdentifiers":[{"nameIdentifier":"63741","nameIdentifierScheme":"WEKO"}],"names":[{"name":"TANAKA, Nozomi"}]},{"nameIdentifiers":[{"nameIdentifier":"63742","nameIdentifierScheme":"WEKO"}],"names":[{"name":"ONO, Takahiro"}]},{"nameIdentifiers":[{"nameIdentifier":"63743","nameIdentifierScheme":"WEKO"}],"names":[{"name":"YAMADA, Kazutoyo"}]},{"nameIdentifiers":[{"nameIdentifier":"63744","nameIdentifierScheme":"WEKO"}],"names":[{"name":"KIKUCHI, Mamoru"}]},{"nameIdentifiers":[{"nameIdentifier":"63745","nameIdentifierScheme":"WEKO"}],"names":[{"name":"TANIGUCHI, Hideo"}]}]},"item_16_publisher_14":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"一般社団法人 日本機械学会"}]},"item_16_relation_26":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_type":"isIdenticalTo","subitem_relation_type_id":{"subitem_relation_type_id_text":"10.1299/kikaib.74.1040","subitem_relation_type_select":"DOI"}}]},"item_16_rights_18":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"©社団法人日本機械学会"}]},"item_16_source_id_9":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0387-5016","subitem_source_identifier_type":"ISSN"}]},"item_16_text_4":{"attribute_name":"著者(機関)","attribute_value_mlt":[{"subitem_text_value":"岩手大学工学部"},{"subitem_text_value":"岩手大学大学院工学研究科"},{"subitem_text_value":"(株)日立グローバルストレージテクノロジーズ"},{"subitem_text_value":"岩手大学工学部"},{"subitem_text_value":"岩手大学工学部"},{"subitem_text_value":"岩手大学工学部"}]},"item_16_version_type_27":{"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":"船崎, 健一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田中, 望"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小野, 隆浩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山田, 和豊"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"菊池, 護"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷口, 英夫"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2016-11-14"}],"displaytype":"detail","filename":"tjsmeb-v74n741p1040-1048.pdf","filesize":[{"value":"1.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"tjsmeb-v74n741p1040-1048.pdf","url":"https://iwate-u.repo.nii.ac.jp/record/10285/files/tjsmeb-v74n741p1040-1048.pdf"},"version_id":"1cd7f3dd-6fdf-45d0-ad5c-ef5b027003cc"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Boundary Layer Measurement","subitem_subject_scheme":"Other"},{"subitem_subject":"Low-Pressure Turbine","subitem_subject_scheme":"Other"},{"subitem_subject":"Separation Bubble","subitem_subject_scheme":"Other"},{"subitem_subject":"Wake Interaction","subitem_subject_scheme":"Other"},{"subitem_subject":"Unsteady Flow","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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"航空エンジン用低圧タービンの高負荷化に関する研究 (wake通過時の剥離を伴う翼面境界層の動的挙動の時間平均的理解)","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航空エンジン用低圧タービンの高負荷化に関する研究 (wake通過時の剥離を伴う翼面境界層の動的挙動の時間平均的理解)"}]},"item_type_id":"16","owner":"3","path":["1519"],"pubdate":{"attribute_name":"公開日","attribute_value":"2013-12-16"},"publish_date":"2013-12-16","publish_status":"0","recid":"10285","relation_version_is_last":true,"title":["航空エンジン用低圧タービンの高負荷化に関する研究 (wake通過時の剥離を伴う翼面境界層の動的挙動の時間平均的理解)"],"weko_creator_id":"3","weko_shared_id":-1},"updated":"2023-05-16T11:39:17.286146+00:00"}