{"created":"2023-06-20T15:07:57.862776+00:00","id":37341,"links":{},"metadata":{"_buckets":{"deposit":"311e97c2-95af-44c0-b81a-10ad93ddc774"},"_deposit":{"created_by":1,"id":"37341","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37341"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037341","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480227","480238","480226","480231","480237","480228","480229","480235","480230","480232","480234","480239","480236","480233"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Comparison between unsteady stage analysis and steady stage analysis for evaluation of aerodynamic performance of single-stage turbine"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"190","bibliographicPageStart":"185","bibliographicVolumeNumber":"41","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所 24-26 Jun. 1998 東京 日本","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory 24-26 Jun. 1998 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"局所時間刻みを用いたレイノルズ平均化3次元ナビエ・ストークスコードを、NALの数値風洞(NWT)と称される並列スーパコンピュータの利用を目的として拡張した。本研究は高圧タービンの静翼の配列について、定常段解析と非定常段解析の比較に注目した。非定常段解析の結果は定常段解析よりも実験結果と良好な一致を与えた。これは、主に、前者の方が後者よりも、ケーシング近傍の2次流についてより良い予測を与えることによる。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A three dimensional time accurate Reynolds-averaged Navier-Stokes code has been extended for use in a parallel supercomputer called Numerical Wind Tunnel (NWT) developed by the Japanese National Aerospace Laboratory. This study focuses on comparison between steady stage analysis and unsteady stage analysis for a stator rotor configuration of a high pressure turbine. The result of the unsteady stage analysis shows better agreement with experimental data than that of the steady stage analysis. This is mainly attributed to better prediction of secondary flow near the casing by the unsteady stage analysis than the steady stage analysis.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001958027","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-41","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"平井, 健二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"児玉, 秀和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大山, 亜希彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野崎, 理"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"菊地, 一雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西澤, 敏雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松尾, 裕一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hirai, Kenji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kodama, Hidekazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oyama, Akihiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nozaki, Osamu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kikuchi, Kazuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishizawa, Toshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuo, Yuichi","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0041027.pdf","filesize":[{"value":"390.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0041027.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37341/files/nalsp0041027.pdf"},"version_id":"73340020-e2fe-462f-86e9-066b8c66e82a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"単段タービン","subitem_subject_scheme":"Other"},{"subitem_subject":"翼列","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常段解析","subitem_subject_scheme":"Other"},{"subitem_subject":"空力性能","subitem_subject_scheme":"Other"},{"subitem_subject":"2次流","subitem_subject_scheme":"Other"},{"subitem_subject":"ケーシング","subitem_subject_scheme":"Other"},{"subitem_subject":"高圧タービン","subitem_subject_scheme":"Other"},{"subitem_subject":"動翼","subitem_subject_scheme":"Other"},{"subitem_subject":"静翼","subitem_subject_scheme":"Other"},{"subitem_subject":"乱流モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"差分法","subitem_subject_scheme":"Other"},{"subitem_subject":"TVDスキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"H型格子","subitem_subject_scheme":"Other"},{"subitem_subject":"全変動減少スキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークスコード","subitem_subject_scheme":"Other"},{"subitem_subject":"single stage turbine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cascade","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady stage analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic performance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"secondary flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"casing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high pressure turbine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rotor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbulence model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"difference method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TVD scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H type lattice","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"total variation diminishing scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes code","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"conference 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