{"created":"2023-06-20T15:08:18.233228+00:00","id":37718,"links":{},"metadata":{"_buckets":{"deposit":"a0cc625d-7784-44d4-80ac-5c4e9fe333e3"},"_deposit":{"created_by":1,"id":"37718","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37718"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037718","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482655","482658","482660","482657","482650","482661","482653","482654","482656","482652","482651","482662","482663","482659"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Application of flow field simulation to turbine vane design"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"180","bibliographicPageStart":"175","bibliographicVolumeNumber":"19","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第10回航空機計算空気力学シンポジウム論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of the NAL symposium on aircraft computational aerodynamics","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 10-12 Jun. 1992 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 10-12 Jun. 1992 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本論文では、タービン静翼翼列の設計への3次元ナビエ・ストークス計算の応用を示す。全圧損失や流出角のような翼列流れ特性の正確な予測は、翼形状の性能を評価するために空力設計者にとって極めて大切である。ここでは、2次流れを抑え圧力損失を軽減するため静翼にlean角やsweep角を与えた場合につき詳細を調べた。3次元ナビエ・ストークス計算に基づく先進的設計法は損失を大幅に軽減することに成功し、設計ツールとしてのコードの有能さを示した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper presents an application of the 3-D Navier-Stokes computations in designing a turbine vane cascade. The accurate prediction of the cascade flow characteristics such as total pressure loss and outlet flow angle is important for aerodynamic engineers to evaluate the performance of airfoil contour shapes. Here curvilinear leaned and swept stator vanes, adopted to suppress the secondary flow and reduce the losses, are studied in detail. The advanced design based on the 3-D Navier-Stokes computations succeeded to reduce the losses greatly showing the capability of the code as a 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: AA0004168032","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-19","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":"石川播磨重工業"},{"subitem_text_value":"石川播磨重工業"},{"subitem_text_value":"石川播磨重工業"},{"subitem_text_value":"石川播磨重工業"},{"subitem_text_value":"石川播磨重工業"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"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":"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"}]},"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":"田中, 厚成"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山脇, るり子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"浜崎, 浩志"}],"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":"Tanaka, Atsushige","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamawaki, Ruriko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hamazaki, Hiroshi","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":"nalsp0019032.pdf","filesize":[{"value":"973.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0019032.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37718/files/nalsp0019032.pdf"},"version_id":"c44d581f-5ba4-4fa9-84e8-dfa0daf93a5f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"タービン静翼","subitem_subject_scheme":"Other"},{"subitem_subject":"空力設計","subitem_subject_scheme":"Other"},{"subitem_subject":"翼列","subitem_subject_scheme":"Other"},{"subitem_subject":"翼列流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"ジェットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"ターボ機械","subitem_subject_scheme":"Other"},{"subitem_subject":"内部流","subitem_subject_scheme":"Other"},{"subitem_subject":"全圧損失","subitem_subject_scheme":"Other"},{"subitem_subject":"流出角","subitem_subject_scheme":"Other"},{"subitem_subject":"3次元ブレード","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD解析","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学解析","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"turbine vane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cascade","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cascade flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"jet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbomachinery","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"internal flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"total pressure loss","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"outlet flow angle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three dimensional blade","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFE analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","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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