{"created":"2023-06-20T15:11:37.972952+00:00","id":41320,"links":{},"metadata":{"_buckets":{"deposit":"9fe554f2-33fa-4388-8dd2-0d1c1e5f27c5"},"_deposit":{"created_by":1,"id":"41320","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41320"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041320","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489465","489464"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Technologies of multidisciplinary simulation for aircraft gas turbine engine"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"104","bibliographicPageStart":"99","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":"本論文では航空用ガスタービン・エンジン開発における総合的なシミュレーションの最近の技術を述べた。そのため、2例を挙げた。最初の例は、到来高速気流応答と空力弾性モード解析に関する非定常空力解析からなるシステムを使用した翼強制応答予測であった。2番目の例は、孔内で作動する回転シャフトをもつ高圧圧縮機の多段ディスクによって形成される多段回転キャビティ内の流れと熱伝達の予測に焦点を当てたものであった。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The paper describes the current technologies of multidisciplinary simulation being used in the aircraft gas turbine engine development. Two sets of examples are presented. The first example is aimed at a prediction of blade forced response using the system which consists of unsteady aerodynamic analysis for incoming gust response and aeroelastic modal analysis. The second example focused the prediction of flow and heat transfer in the multiple rotating cavities formed by the multiple discs of the HP (High Pressure) compressor with a rotating shaft running through the bores.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635019","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":"石川島播磨重工業"}]},"item_3_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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"児玉, 秀和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kodama, Hidekazu","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":"nalsp0046019.pdf","filesize":[{"value":"494.1 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0046019.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41320/files/nalsp0046019.pdf"},"version_id":"b3520492-6368-4297-8891-78085f049586"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"航空用エンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"ガスタービン","subitem_subject_scheme":"Other"},{"subitem_subject":"総合シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"到来高速気流応答","subitem_subject_scheme":"Other"},{"subitem_subject":"空力弾性モード解析","subitem_subject_scheme":"Other"},{"subitem_subject":"非定常空力解析","subitem_subject_scheme":"Other"},{"subitem_subject":"翼強制応答","subitem_subject_scheme":"Other"},{"subitem_subject":"高圧圧縮機","subitem_subject_scheme":"Other"},{"subitem_subject":"多段ディスク","subitem_subject_scheme":"Other"},{"subitem_subject":"多段回転キャビティ","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ予測","subitem_subject_scheme":"Other"},{"subitem_subject":"熱伝達","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gas turbine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multidisciplinary simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"incoming gust response","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroelastic modal analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unsteady aerodynamic analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"blade forced response","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high pressure compressor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiple disc","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiple rotating cavity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow prediction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat transfer","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"航空用エンジンにおける統合シミュレーション技術","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航空用エンジンにおける統合シミュレーション技術"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41320","relation_version_is_last":true,"title":["航空用エンジンにおける統合シミュレーション技術"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:03:17.991963+00:00"}