{"created":"2023-06-20T15:05:16.852943+00:00","id":34569,"links":{},"metadata":{"_buckets":{"deposit":"f4d2f37a-4438-4da6-9c62-1678eaa7b469"},"_deposit":{"created_by":1,"id":"34569","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"34569"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00034569","sets":["1887:1890","1896:1898:1899:1992"]},"author_link":["419884","419885"],"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1981-02","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"3","bibliographicPageEnd":"103","bibliographicPageStart":"93","bibliographicVolumeNumber":"46","bibliographic_titles":[{},{"bibliographic_title":"ISAS report/Institute of Space and Aeronautical Science,University of Tokyo","bibliographic_titleLang":"en"}]}]},"item_9_description_17":{"attribute_name":"抄録(英)","attribute_value_mlt":[{"subitem_description":"Nonuniformity of inlet flows through a test compressor stage has been studied based upon 3-D semi-actuator disk theory. The results show that the rotor blade vibration greatly influences the attenuation rate of distortion. The effects of the rotor/stator separation, the circumferential modal index and the tilting of the inlet distortion, are also demonstrated.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA2401428000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_publisher_9":{"attribute_name":"出版者(英)","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Aeronautical Science,University of Tokyo"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0372-1418","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA00675986","subitem_source_identifier_type":"NCID"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"TANIDA, Yoshimichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAGASHIMA, Toshio","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":"2020-01-24"}],"displaytype":"detail","filename":"SA2401428.pdf","filesize":[{"value":"577.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA2401428.pdf","url":"https://jaxa.repo.nii.ac.jp/record/34569/files/SA2401428.pdf"},"version_id":"41865e54-bb37-44d0-a89c-2bcb70e50ca8"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"Inlet Distortion and Blade Vibration in Turbomachines","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Inlet Distortion and Blade Vibration in Turbomachines","subitem_title_language":"en"}]},"item_type_id":"9","owner":"1","path":["1890","1992"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"34569","relation_version_is_last":true,"title":["Inlet Distortion and Blade Vibration in Turbomachines"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T23:39:21.098046+00:00"}