{"created":"2023-06-20T15:11:43.152064+00:00","id":41432,"links":{},"metadata":{"_buckets":{"deposit":"323a2702-b7a0-4d95-bc6e-aae6a7ed9938"},"_deposit":{"created_by":1,"id":"41432","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41432"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041432","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["490010","490008","490007","490009","490006","490011"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"非構造格子アプローチによる随伴法を用いた超音速翼・ナセル形状の空力最適化"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"129","bibliographicPageStart":"121","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":"空力設計法を、3次元非構造オイラーコードと離散アプローチの随伴コードを用いて開発してきた。得られた随伴コードは、翼・機体・ナセル形状の超音速輸送機の翼設計問題に適用される。Hicks-Henne形状関数を表面幾何学形状の摂動に用い、設計過程において楕円方程式法を内部格子の修正に用いた。ナセルの平行移動に伴う設計パラメータを除いて、内部格子の感度は無視した。逐次2次プログラミング法を揚力や翼厚に対する拘束を保持しながら抗力を最小にすることに用いた。良好な設計結果は、この設計方法の正当性と有効性を確認した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An aerodynamic design method has been developed by using a three-dimensional unstructured Euler code and an adjoint code with a discrete approach. The resulting adjoint code is applied to a wing design problem of supersonic transport with a wing-body-nacelle configuration. Hicks-Henne shape functions are adopted for the surface geometry perturbation, and the elliptic equation method is employed for the interior grid modification during the design process. Interior grid sensitivities are neglected except those for design parameters associated with nacelle translation. The sequential quadratic programming method is used to minimize the drag with constraints on the lift and airfoil thickness. Successful design results confirm validity and efficiency of the present design method.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028638016","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":"東北大学 大学院工学研究科"},{"subitem_text_value":"東北大学 大学院工学研究科"},{"subitem_text_value":"東北大学 大学院工学研究科"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School of Engineering"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Kim, Hyoung-Jin"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大林, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中橋, 和博"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kim, Hyoung-Jin","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Obayashi, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakahashi, Kazuhiro","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":"nalsp0049016.pdf","filesize":[{"value":"946.1 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0049016.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41432/files/nalsp0049016.pdf"},"version_id":"249d0332-c309-487f-9a42-c8e83d5f86a0"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"空力最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"翼・ナセル形状","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"非構造格子オイラーコード","subitem_subject_scheme":"Other"},{"subitem_subject":"随伴法","subitem_subject_scheme":"Other"},{"subitem_subject":"Hicks-Henne形状関数","subitem_subject_scheme":"Other"},{"subitem_subject":"楕円方程式法","subitem_subject_scheme":"Other"},{"subitem_subject":"逐次2次プログラミング法","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing nacelle configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unstructured grid Euler code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"adjoint method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hicks Henne shape function","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"elliptic equation method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sequential quadratic programming method","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":"Aerodynamic optimization of supersonic wing-nacelle configuration using an adjoint method with the unstructured-grid approach","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Aerodynamic optimization of supersonic wing-nacelle configuration using an adjoint method with the unstructured-grid approach","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":"41432","relation_version_is_last":true,"title":["Aerodynamic optimization of supersonic wing-nacelle configuration using an adjoint method with the unstructured-grid approach"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:00:21.933578+00:00"}