{"created":"2023-06-20T15:15:04.535375+00:00","id":45123,"links":{},"metadata":{"_buckets":{"deposit":"510437e1-ca8d-40c6-91ae-f0af2dfaa349"},"_deposit":{"created_by":1,"id":"45123","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45123"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045123","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["473034","473036","473033","473035"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Analysis of Two-Dimensional Turbine Cascade Flow By Finite Area Method (Comparison of Numerical and Experimental Results)"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1985-07","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"12","bibliographicVolumeNumber":"865","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-865","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"当所において作成した有限面積法による二次元翼間流れ解析のプログラムの汎用化の検討を遷音速タービン翼列を用いて,流出マッハ数と流入角を変えて数値解析し,実験結果と比較を行いその実用性について検討した。その結果,強い衝撃波の発生しない領域で実用性のあるプログラムであることを確認した。また,解の性質についての検討も行った。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A two-dimensional time marching blade-to-blade flow analysis program was employed to analyse the transonic turbine cascade flows. The transonic turbine cascade flows are numerically calculated for several outlet Mach numbers and inlet angles. The computed airfoil pressure distributions have been compared with the experimantal results. The comparison shows excellent agreement for subcritical and supercritical flow with weak shock wave.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0865000","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-865","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":"橋本, 良作"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西村, 英明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HASHIMOTO, Ryosaku","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NISHIMURA, Hideaki","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":"naltr00865.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00865.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45123/files/naltr00865.pdf"},"version_id":"a461625c-c690-4bd4-a2c3-85aad15522c8"}]},"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":"有限面積法による非粘性二次元翼列解析(実験と数値計算の検証例)","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"有限面積法による非粘性二次元翼列解析(実験と数値計算の検証例)"}]},"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":"45123","relation_version_is_last":true,"title":["有限面積法による非粘性二次元翼列解析(実験と数値計算の検証例)"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:44:53.979361+00:00"}