{"created":"2023-06-20T15:11:42.740141+00:00","id":41423,"links":{},"metadata":{"_buckets":{"deposit":"6cf8c62b-21ff-497c-876c-0c78f7222e5b"},"_deposit":{"created_by":1,"id":"41423","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41423"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041423","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489951"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"最新航空機の設計への先進的CFD手法の応用"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"71","bibliographicPageStart":"61","bibliographicVolumeNumber":"49T","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 17-19 Jan. 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 17-19 Jan. 2000 Tokyo Japan","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航空機設計は風洞試験に基づいて行い、最終的な検証を飛行試験で行うのが従来の手法であった。1960年代後期にCFD(計算流体力学)が出現した。計算機の速度および記憶容量が増加するにつれて、航空機設計におけるCFDの役割が着実に増加した。今日、CFDは風洞試験および飛行試験とともに主要な空力技術となっている。リスクを減らし、低コストで優れた性能を達成するにはこれらの技術それぞれに最新の技術能力が必要である。本報ではBombardierのビジネスジェットおよび地域ジェットへの応用を例に説明し、高性能ジェット機の空力技術開発におけるCFDの役割を考察した。重点を手法におき、特に、最適形態に到達するためのCFDと目標を絞った風洞試験および飛行試験との組合せに重点を置いた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The approach to aircraft design has traditionally been based on wind tunnel testing with flight testing being used for final validation. CFD (Computational Fluid Dynamics) emerged in the late 1960's. Its role in aircraft design increased steadily as speed and memory of computers increased. Today CFD is a principal aerodynamic technology along with wind tunnel testing and flight testing. State of the art capabilities in each of these technologies are needed to achieve superior performance with reduced risk and low cost. This paper discusses the role of CFD in the aerodynamic development of high performance jets, as illustrated by the application to Bombardier Business and Regional Jets. Emphasis is put on the methodology, in particular the combination of CFD with targeted wind tunnel tests and flight tests to arrive at optimal configurations.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028638007","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-49T","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":"Bombardier Aerospace Advanced Aerodynamics"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Bombardier Aerospace Advanced Aerodynamics"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Kafyeke, Fassi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"489951","nameIdentifierScheme":"WEKO"}]}]},"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":"nalsp0049007.pdf","filesize":[{"value":"3.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0049007.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41423/files/nalsp0049007.pdf"},"version_id":"bb0e08f7-adbf-48c0-895e-153333c109a7"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"最新航空機","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":"航空機設計","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行試験","subitem_subject_scheme":"Other"},{"subitem_subject":"最適形態","subitem_subject_scheme":"Other"},{"subitem_subject":"設計環境","subitem_subject_scheme":"Other"},{"subitem_subject":"modern airplane","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":"aircraft design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optimal configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"design environment","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Application of advanced CFD methods to the design of modern airplanes","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Application of advanced CFD methods to the design of modern airplanes","subitem_title_language":"en"}]},"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":"41423","relation_version_is_last":true,"title":["Application of advanced CFD methods to the design of modern airplanes"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:00:33.904319+00:00"}