{"created":"2023-06-20T15:15:11.619395+00:00","id":45243,"links":{},"metadata":{"_buckets":{"deposit":"8686b8ea-77b6-4427-b370-72ddaeb00573"},"_deposit":{"created_by":1,"id":"45243","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45243"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045243","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["473675","473673","473676","473674"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1988-06","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"24","bibliographicVolumeNumber":"984T","bibliographic_titles":[{},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-984T","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本論文は低速直線タービン動翼列内で生ずる三次元流とそれに伴う損失に及ぼすインシデンスの影響について述べたものである。7.2度から－53.3度の異なる5種類のインシデンスについて,翼列の流れを翼列の軸方向に配置した15又は16個の断面で詳細に測定した。翼スパン中央や翼端面近傍の翼間面(blade-to-blade)上の流れ,翼表面に沿う子午面(meridional)流れ,翼間での静圧あるいは全圧分布を解析した。その結果は非常に複雑な翼間での流れや損失発生メカニズムを容易に理解できるように,速度ベクトル,スカラー量の等高線,さらに流線を用いて三次元表示した。本研究はインシデンスの影響に関する新しい知見を与えるのみならず,既に知られ又は推定されている知識にも多くの確固とした実験事実を与えるものである。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The paper describes effects of the incidence on cascade three-dimensional flows and on the associated loss mechanism occurring in a low-speed linear turbine rotor cascade. For five different incidences from 7.2 to -53.3 degrees, the cascade flow was surveyed in detail at fifteen or sixteen planes located axially throughout the cascade. Blade-to-blade flows at the cascade midspan and near the endwalls, meridional flows along the blade surfaces, and static and total pressures within the cascade were analized and the results were represented in three-dimensional forms using vectors, scalar contours and streaklines, from which one could easily understand the extraordinarily complicated cascade flows and the loss generation mechanisms. The present study gives not only new insight into the incidence effects but also adds many solid experimental facts in a quantitative manner to our knowledge of turbine cascade flows.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0984000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-984T","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所原動機部"},{"subitem_text_value":"航空宇宙技術研究所原動機部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aeroengine Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Aeroengine Division, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山本, 孝正"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"能瀬, 弘幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"YAMAMOTO, Atsumasa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NOUSE, 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":"2020-01-29"}],"displaytype":"detail","filename":"naltr0984t.pdf","filesize":[{"value":"2.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0984t.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45243/files/naltr0984t.pdf"},"version_id":"ad6e83df-36f7-44c4-a2d7-ec39402dd3a2"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"Three-Dimensional Flows and Loss Generation Mechanisms In a Linear Turbine Rotor Cascade at Various Incidence Cinditions","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Three-Dimensional Flows and Loss Generation Mechanisms In a Linear Turbine Rotor Cascade at Various Incidence Cinditions","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"45243","relation_version_is_last":true,"title":["Three-Dimensional Flows and Loss Generation Mechanisms In a Linear Turbine Rotor Cascade at Various Incidence Cinditions"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:42:47.963579+00:00"}