{"created":"2023-06-20T15:08:24.028260+00:00","id":37839,"links":{},"metadata":{"_buckets":{"deposit":"9e38b4f9-bef0-4c75-b61b-1fea79a830f4"},"_deposit":{"created_by":1,"id":"37839","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37839"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037839","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["430549","430546","430547","430550","430545","430542","430551","430543","430544","430548"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Design of secondary flow control cascade using numerical simulation"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"55","bibliographicPageStart":"51","bibliographicVolumeNumber":"27","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_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"軸流ターボ機械設計の傾向は、より高いブレード負荷をめざす方向にあり、2次流れの効果とそれに結びついた損失とが重要視されている。高速の圧縮機翼列におけるこのような複雑な3次元流れの計測は極めて難しいことが示されており、他方、高度化された数値シミュレーションによれば、これらの流れや損失を首尾よく予測することが可能である。本論文では、数値シミュレーションを用いて、圧縮機静翼の翼端領域における2次流れと損失の低減を狙った設計の結果を示す。リグ試験により得られた結果との比較も示した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The trend of axial turbomachine design is toward higher blade loadings which places more emphasis on secondary flow effects and the associated losses. Measurements of these complex three-dimensional flows in high speed compressor cascades have proven to be very difficult. On the other hand, a sophisticated numerical simulation can predict these flows and the losses successfully. This paper presents the results of a design which aim to reduce secondary flow and the losses at endwall regions of compressor stators, using numerical simulations. A comparison with the results obtained in rig tests will be also presented.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004174002","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-27","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":"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":"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":"大北, 洋治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"児玉, 秀和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"菊地, 一雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野崎, 理"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田村, 敦宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Okita, Yoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kodama, Hidekazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kikuchi, Kazuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nozaki, Osamu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tamura, Atsuhiro","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":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0027002.pdf","filesize":[{"value":"377.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0027002.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37839/files/nalsp0027002.pdf"},"version_id":"8b1b1717-e6e1-4ac4-a09c-557e927647c4"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"翼列設計","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮機静翼設計","subitem_subject_scheme":"Other"},{"subitem_subject":"内部流解析","subitem_subject_scheme":"Other"},{"subitem_subject":"翼列2次流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮機翼端部流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"翼列損失","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ･ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD対風洞相関","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"cascade design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressor stator design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"internal flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cascade secondary flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressor endwall flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cascade loss","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD wind tunnel correlation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","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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