{"created":"2023-06-20T15:07:31.737533+00:00","id":36893,"links":{},"metadata":{"_buckets":{"deposit":"65e73e19-61ed-4fa3-83e8-22cfa4d6df23"},"_deposit":{"created_by":1,"id":"36893","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36893"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036893","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["478071","478080","478077","478075","478076","478074","478078","478079","478073","478069","478070","478072"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Unsteady single stage analysis for a high pressure turbine"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"194","bibliographicPageStart":"189","bibliographicVolumeNumber":"34","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 6-7 JUN. 1996 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 6-7 JUN. 1996 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"静翼列と動翼列からなる高圧タービン単段翼列配列を通る流れの数値シミュレーションを行った。単段翼列配列の非定常空力特性を評価するために、非定常アルゴリズム、ブロック構造格子システム、スライド格子手法を用いて3次元ナビエ・ストークスコードを開発し、検証計算を行った。ステージの空力性能を評価するために、静翼1翼間と回転する動翼2翼間を通る単純化した流れ場を同時に計算した。数値結果は、圧力損失係数、ステージ全効率などの実験データとかなりよく一致し、空力設計ツールとしての数値コードの有用性を立証した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The flows through a single stage high pressure turbine cascade configuration, consisting of a stator vane cascade and a rotor blade cascade, were numerically simulated. A 3-D Navier-Stokes code, using unsteady algorithm, block structure grid system and sliding grid technique, was developed and verified here to estimate the unsteady aerodynamic characteristics of the single stage cascade configuration. The simplified flowfield through one stator vane passage and moving two rotor blade passages were calculated simultaneously here to evaluate the aerodynamic performances of the stage. The numerical results showed a fairly good agreement with experimental data, such as pressure loss coefficients and stage total efficiencies, demonstrating the effectiveness of the numerical code as an aerodynamic design tool.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000685034","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-34","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"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"松永, 康二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"竹内, 久雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"平井, 健二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松尾, 裕一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"菊地, 一雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野崎, 理"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsunaga, Koji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takeuchi, Hisao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hirai, Kenji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuo, Yuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kikuchi, Kazuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nozaki, Osamu","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":"nalsp0034034.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0034034.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36893/files/nalsp0034034.pdf"},"version_id":"d5bd7194-22d5-484e-b6cf-42a2904b924f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"高圧タービン","subitem_subject_scheme":"Other"},{"subitem_subject":"単段流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"静翼列","subitem_subject_scheme":"Other"},{"subitem_subject":"動翼列","subitem_subject_scheme":"Other"},{"subitem_subject":"3次元ナビエ・ストークスコード","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常流れ解析コード","subitem_subject_scheme":"Other"},{"subitem_subject":"ブロック構造格子","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力損失係数","subitem_subject_scheme":"Other"},{"subitem_subject":"ステージ全効率","subitem_subject_scheme":"Other"},{"subitem_subject":"high pressure turbine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"single stage flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stator vane cascade","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rotor blade cascade","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three dimensional Navier Stokes code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady flow analysis code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"block structure grid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure loss coefficient","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stage total efficiency","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 paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"タービン単段流れの数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"タービン単段流れの数値シミュレーション"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"36893","relation_version_is_last":true,"title":["タービン単段流れの数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:29:37.846640+00:00"}