{"created":"2023-06-20T15:11:39.087613+00:00","id":41343,"links":{},"metadata":{"_buckets":{"deposit":"4d4bb23a-aeb3-4dea-b79a-679028f2cd1c"},"_deposit":{"created_by":1,"id":"41343","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41343"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041343","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489585","489584","489589","489588","489590","489587","489586","489581","489580","489582","489591","489583","489578","489579"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"On development of CFD platform for blade rows"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"236","bibliographicPageStart":"231","bibliographicVolumeNumber":"46","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_3_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 7-9 Jun. 2000 東京 日本","subitem_description_type":"Other"}]},"item_3_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 7-9 Jun. 2000 Tokyo Japan","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本論文では、航空機エンジン、船舶、発電所のターボ機械の空力設計技術者のために効率的な技術環境を実現する翼列設計用のCFD(計算流体力学)プラットフォームについて解説した。プラットフォームをネットワークで接続したPC、ワークステーション(WS)、スーパコンピュータから構成した。このプラットフォームでは設計者が計算グリッドを生成したり、流体計算をしたり、計算結果を解析、視覚化する際に、その操作が容易になる様、CFDプログラムをこれらのコンピュータで運用するためのグラフィックユーザインタフェースを提供した。また、翼列の幾何学的形状のようなデータや、計算した流体のデータの様に空力性能を比較したり、翼列の設計を評価するのに必要なデータをデータベースに保存したり、参照したりする機能も保持した。本稿では、2次元の翼列のために開発したプラットフォームのプロトタイプを紹介した。多段ターボ機械のための流体解法コードも並列計算ライブラリとともに開発し、このプラットフォームに取り込んだ。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The present paper shows a CFD (Computational Fluid Dynamics) platform for blade rows, which realize efficient engineering environment for aerodynamic designers of turbomachine for aircraft engines, ships and electric power plants. The platform consists of PCs, WSs (Workstations) and supercomputers on network. It provides graphic user interfaces on these computers to control the CFD programs, so that the designers can operate very easily their tasks such as generating the computational grids, calculating the flow, and analyzing/visualizing the computed results. It also has the functions to save/restore in the database such data as geometric profiles of blade rows, computed data of the flow, which data are necessary to compare the aerodynamic performance and estimate the design of blade row. In this paper, a prototype platform is demonstrated, which has been developed by the authors for two-dimensional blade rows. A flow solver for a multi-stage turbomachine is also developed with parallel computing library and incorporated in this platform.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635042","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-46","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_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_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"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"},{"subitem_text_value":"富士総合研究所"},{"subitem_text_value":"富士総合研究所"},{"subitem_text_value":"富士総合研究所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"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"},{"subitem_text_language":"en","subitem_text_value":"Fuji Research Institute Corporation"},{"subitem_text_language":"en","subitem_text_value":"Fuji Research Institute Corporation"},{"subitem_text_language":"en","subitem_text_value":"Fuji Research Institute Corporation"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"西澤, 敏雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野崎, 理"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 孝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"福田, 正大"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"加藤, 昭史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"助村, 俊一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"川崎, 琢治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishizawa, Toshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nozaki, Osamu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fukuda, Masahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kato, Akifumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sukemura, Shuniti","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawasaki, Takuji","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":"nalsp0046042.pdf","filesize":[{"value":"1.7 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row","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turbomachine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electric power plant","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"graphic user interface","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"parallel computing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD platform","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"engineering 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