{"created":"2023-06-20T15:13:56.232742+00:00","id":43906,"links":{},"metadata":{"_buckets":{"deposit":"f8aade57-819d-4ff6-acd2-69f5afda49df"},"_deposit":{"created_by":1,"id":"43906","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43906"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043906","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["466261","466262","466258","466259","466260","466257"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"An Analytical Method of Evaluating the Effect of Coolig-Air on Air-Cooled Turbine Performance Utilizing the Small-Deviation Method"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1976-12","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"21","bibliographicVolumeNumber":"323","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper presents a simple analytical method for air cooled turbine performance utilizing the small deviation method. The new method has many advantages, the most outstanding of which is the capability of calculating the effects of cooling air on various parameters of turbine performance in a simple manner. Various functional relationships, including cooling air flow rate and change of Row path area etc., are derived for the two-stage turbine employed as the example turbine to show the calculation procedure of the present method.  The method was also compared with available experimental data on single-stage tur- bines. The comparison showed good agreement.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0323000","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 TM-323","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":"0452-2982","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00314334","subitem_source_identifier_type":"NCID"}]},"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"},{"subitem_text_value":"航空宇宙技術研究所原動機部"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山本, 孝正"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高原, 北雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"臼井, 弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"YAMAMOTO, Atsumasa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TAKAHARA, Kitao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"USUI, Hiroshi","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":"2020-01-28"}],"displaytype":"detail","filename":"naltm00323.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00323.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43906/files/naltm00323.pdf"},"version_id":"3ef8b604-c343-4d43-a800-30cbc780760f"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"Small Devition法による空冷タービンの空力性能に及ぼす冷却空気の影響の解析法","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Small Devition法による空冷タービンの空力性能に及ぼす冷却空気の影響の解析法"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43906","relation_version_is_last":true,"title":["Small Devition法による空冷タービンの空力性能に及ぼす冷却空気の影響の解析法"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:05:50.799956+00:00"}