{"created":"2023-06-20T15:08:18.136505+00:00","id":37716,"links":{},"metadata":{"_buckets":{"deposit":"03e233d7-f78d-4c9d-b1c1-a4953961f2ef"},"_deposit":{"created_by":1,"id":"37716","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37716"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037716","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482645","482644","482642","482643","482641","482635","482636","482637","482639","482640","482638","482634"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Verification of a three-dimensional viscous flow analysis for a single stage compressor"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"168","bibliographicPageStart":"163","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":"高負荷単段軸流圧縮機ロータブレードまわりの遷音速流れ場を、Chakravathy-Osher型TVD(全変動減少型)スキームを用いた3次元ナビエ・ストークス方程式コードにより数値的に調べた。IGV(入口案内翼)およびロータブレードのまわりの流れを同時に計算する段間解析を実施した。設計値および実験データと比較すると、計算は量的にやや異なった結果を与える。しかしながら、数値計算結果は圧縮機の圧力上昇特性および強い衝撃波を含む流れのパターンをよくシミュレートする。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A transonic flowfield around rotor blades of a highly loaded single stage axial compressor was numerically analyzed by a three-dimensional compressible Navier-Stokes equations code using Chakravarthy and Osher type TVD (Total Variation Diminishing) scheme. A stage analysis which calculates both flowfields around IGV (Inlet Guide Vane) and rotor blades simultaneously was carried out. Comparing with design values and experimental data, computed results gave slight difference quantitatively. But the results of numerical calculation simulated well pressure rise characteristics of compressor and its flow pattern including strong shock surface.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004168030","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":"川崎重工業"},{"subitem_text_value":"川崎重工業"},{"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":"Kawasaki Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries 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":"松岡, 右典"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋本, 啓介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野崎, 理"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"菊地, 一雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"福田, 正大"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田村, 敦宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuoka, Akinori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hasimoto, Keisuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nozaki, Osamu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kikuchi, Kazuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fukuda, Masahiro","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0019030.pdf","filesize":[{"value":"445.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0019030.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37716/files/nalsp0019030.pdf"},"version_id":"545d68a9-7b59-48e4-b41f-085f4301a21a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"翼列流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮機","subitem_subject_scheme":"Other"},{"subitem_subject":"空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"ロータブレード","subitem_subject_scheme":"Other"},{"subitem_subject":"ジェットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"軸流圧縮機","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速翼列","subitem_subject_scheme":"Other"},{"subitem_subject":"入口案内翼","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮機段","subitem_subject_scheme":"Other"},{"subitem_subject":"内部流","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":"cascade flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rotor blade","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"jet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"axial compressor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic cascade","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inlet guide vane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressor stage","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"internal flow","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":"CFD 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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