{"created":"2023-06-20T15:07:30.570041+00:00","id":36876,"links":{},"metadata":{"_buckets":{"deposit":"81a5f87c-6d9a-4729-b46a-d78480757960"},"_deposit":{"created_by":1,"id":"36876","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36876"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036876","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477957","477961","477962","477959","477958","477960"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"An inverse design method for multiple wing systems with interaction"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"94","bibliographicPageStart":"89","bibliographicVolumeNumber":"34","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_5_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 6-7 JUN. 1996 東京 日本","subitem_description_type":"Other"}]},"item_5_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 6-7 JUN. 1996 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"多翼(あるいは多翼素翼)を扱う逆設計法を設計断面形状に及ぼす翼間の相互干渉の影響の観点から検討した。この新規方法は高梨の積分方程式法を基にして考案した。指定された表面圧力分布を与える翼の断面形状を与えるため翼間の相互干渉を考慮に入れた。この方法はいくつかの予備的設計問題にうまく対応した。効率的で精密な設計のためには、空力的相互干渉、およびある翼の幾何学的変化と他の翼の変化との間の相関の両方を考慮しなければならないことが分かった。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An inverse design method that treats multiple wings (or multi components of a wing) is examined from the viewpoint of the effect of interaction among wings on a designed section shape. This new method has been devised recently on the basis of Takanashi's integral equation method. It takes into consideration the mutual interaction among wings to provide section shapes of wings which realize a specified surface pressure distribution. This method works well on several preliminary design problems. It is found that both of aerodynamic mutual interaction and the correlation between the geometrical change of a certain wing and that of the others should be considered for efficient and accurate design.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000685017","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-34","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_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_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"富士通"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fujitsu Limited"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"松島, 紀佐"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高梨, 進"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩宮, 敏幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsushima, Kisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takanashi, Susumu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwamiya, Toshiyuki","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":"nalsp0034017.pdf","filesize":[{"value":"707.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0034017.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36876/files/nalsp0034017.pdf"},"version_id":"8cf65b3c-5405-47b0-89a9-77b674be6543"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"逆問題解法","subitem_subject_scheme":"Other"},{"subitem_subject":"多翼系","subitem_subject_scheme":"Other"},{"subitem_subject":"相互干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"翼断面形状","subitem_subject_scheme":"Other"},{"subitem_subject":"逆問題","subitem_subject_scheme":"Other"},{"subitem_subject":"表面圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークスシミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"inverse design method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiple wing system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mutual interaction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing section shape","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inverse problem","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"surface pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes simulation","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"相互干渉を考慮した多翼系の逆問題解法","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"相互干渉を考慮した多翼系の逆問題解法"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"36876","relation_version_is_last":true,"title":["相互干渉を考慮した多翼系の逆問題解法"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:30:03.204041+00:00"}