{"created":"2023-06-20T15:11:43.709469+00:00","id":41444,"links":{},"metadata":{"_buckets":{"deposit":"7e272406-9086-499c-a46a-415c14732bc2"},"_deposit":{"created_by":1,"id":"41444","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41444"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041444","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["490056","490058","490057","490059"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"超音速実験機の空力設計にCFD解析を応用したいくつかの事例"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"202","bibliographicPageStart":"193","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":"1997年、航空宇宙技術研究所(NAL)は、次世代超音速輸送機開発のための技術的基盤の確立を目的に、縮尺超音速実験機を開発する計画を開始した。2002年の初実験飛行に向けて無動力実験機の開発が進められている。実験機をロケットブースタにより打ち上げる。ロケットブースタを分離の後、実験機はマッハ数2.0、高度18.5kmで計測飛行を開始する。実験機の空力設計において、三菱重工業(株)(MHI)は全体設計を担当し、NALはその高度なCFD(計算流体力学)コードを用いて主に翼および翼-胴空力接合の設計を行った。また、MHIは打上げ形態の空力設計を担当した。MHIの設計作業においては、風洞試験データを主に使用した。実験データのいくつかを検討し、CFD解析を用いて修正した。さらに、実験機およびロケットブースタの複雑な流れ場の物理的現象を理解する上で、CFD解析が重要な役割を果たした。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In 1997, National Aerospace Laboratory (NAL) started a program to develop a scaled supersonic experimental airplane to establish the technological basis for the development of the next generation supersonic transport. A non-powered experimental airplane is being developed for the first experimental flight in 2002. The airplane is launched by a rocket-booster. After the rocket-booster is separated, the airplane starts the measurement flight at Mach 2.0 and altitude 18.5 km. In the aerodynamic design of the experimental airplane, Mitsubishi Heavy Industries, Ltd. (MHI) is in charge of the overall design and NAL mainly conducted the wing and wing-body aerodynamic integration design with their sophisticated CFD (Computational Fluid Dynamics) code. MHI is also in charge of the launch configuration aerodynamic design. In the MHI design work, wind tunnel test data were mainly used. Some experimental data were checked and corrected using the CFD analysis. CFD analysis also played an important role in understanding physical phenomena of the complicated flow field of the experimental airplane and the rocket-booster.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028638028","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":"三菱重工業"},{"subitem_text_value":"三菱重工業"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"二ツ寺, 直樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"海田, 武司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Futatsudera, Naoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kaiden, Takeshi","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":"nalsp0049028.pdf","filesize":[{"value":"3.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0049028.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41444/files/nalsp0049028.pdf"},"version_id":"e86c06e0-a3f9-48fd-b307-4db524bdbd91"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"航空力学設計","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速実験飛行機","subitem_subject_scheme":"Other"},{"subitem_subject":"ロケットブースタ","subitem_subject_scheme":"Other"},{"subitem_subject":"ヒンジモーメント","subitem_subject_scheme":"Other"},{"subitem_subject":"発射形態","subitem_subject_scheme":"Other"},{"subitem_subject":"干渉抗力","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic experimental airplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rocket booster","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hinge moment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"launch configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"interference force","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":"Some practical applications of CFD analysis to aerodynamic design of the supersonic experimental airplane","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Some practical applications of CFD analysis to aerodynamic design of the supersonic experimental airplane","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":"41444","relation_version_is_last":true,"title":["Some practical applications of CFD analysis to aerodynamic design of the supersonic experimental airplane"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:00:05.896416+00:00"}