{"created":"2023-06-20T15:15:00.588555+00:00","id":45042,"links":{},"metadata":{"_buckets":{"deposit":"a572eec5-1d35-41bf-b22f-dd44ad4ad095"},"_deposit":{"created_by":1,"id":"45042","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45042"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045042","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["472618","472619","472621","472620"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Evaluation of thermocouple and thermal radiation instrumentation for measuring gas turbine combustor liner temperature"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1983-11","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"12","bibliographicVolumeNumber":"784","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-784","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Temperature measurement techniques for a practical combustion chamber liner wall were investigated. Fourteen ways of sheathed thermocouple installations on thin stainless steel plated simulating a combustor liner wall were tested by flowing a hot gas on one side and cold air on the other side under atmospheric conditions. Temperature ranges of the hot gas and the cold air were 542～612K and 317～326K, respectively. The tested stream velocities were in the ranges of 70～87m/s for the hot gas and 14～70m/s for the cold gas. It was found that Reynolds numbers of the hot and cold streams have no significant effects on the magnitude of the error and that only the method of installation determines the accuracy of the measurements. It was also found that radiation measurements of the black coated wall surface may cause significant error because there is a big temperature gradient across the coating layer.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0784000","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-784","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":"田丸, 卓"}],"nameIdentifiers":[{"nameIdentifier":"472618","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"黒沢, 要治"}],"nameIdentifiers":[{"nameIdentifier":"472619","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"TAMARU, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"472620","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"KUROSAWA, Yoji","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"472621","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr00784.pdf","filesize":[{"value":"873.5 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00784.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45042/files/naltr00784.pdf"},"version_id":"0cc2827c-fa37-4010-b65c-fa893db27250"}]},"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":"ガスタービン燃焼器ライナ壁温測定のための熱電対取付法,および輻射計測法の評価","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ガスタービン燃焼器ライナ壁温測定のための熱電対取付法,および輻射計測法の評価"}]},"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":"45042","relation_version_is_last":true,"title":["ガスタービン燃焼器ライナ壁温測定のための熱電対取付法,および輻射計測法の評価"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:46:20.332473+00:00"}