{"created":"2023-06-20T15:08:01.022221+00:00","id":37405,"links":{},"metadata":{"_buckets":{"deposit":"f58d1a5c-c538-4026-911a-a830a822b967"},"_deposit":{"created_by":1,"id":"37405","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37405"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037405","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480609","480615","480611","480614","480613","480610","480608","480612"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Natural laminar flow wing design of NAL's scaled supersonic experimental airplane"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"28","bibliographicPageStart":"25","bibliographicVolumeNumber":"43","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publicationa 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 7-9 Oct. 1998 (23th). 24-26 Mar. 1999 (24th) 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 7-9 Oct. 1998 (23th). 24-26 Mar. 1999 (24th) Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"NALでは無推進小型超音速実験機の空力形状を設計したところである。超音速での抵抗を減らすため、平面形アロー翼、ワープ翼、面積法則を適用した胴体、および自然層流(NLF)翼というデザインの考え方を採用した。NLF翼の設計のために、最適な圧力分布をサリーコードを用いて調べ、CFD(数値流体力学)逆問題設計法を独自に開発した。設計された翼は大きな層流領域を持つと推定した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"NAL has just designed an aerodynamic configuration of the un-powered scaled supersonic experimental airplane. The following design concepts for reducing supersonic drag were incorporated: arrow planform, warp, area-ruled body and Natural Laminar Flow (NLF) wing. For the NLF wing design, an optimum design pressure distribution was investigated using SALLY code and a new inverse design method with CFD was originally developed. The designed wing was estimated to have large laminar region.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001960008","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-43","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":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"富士通"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"Fujitsu Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"吉田, 憲司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"真保, 雄一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩宮, 敏幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松島, 紀佐"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshida, Kenji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shinbo, Yuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwamiya, Toshiyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsushima, Kisa","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":"nalsp0043008.pdf","filesize":[{"value":"779.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0043008.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37405/files/nalsp0043008.pdf"},"version_id":"d1357c45-dc90-4173-a2b9-b0122fb7ed53"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"境界層遷移","subitem_subject_scheme":"Other"},{"subitem_subject":"横流れ不安定","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD逆問題法","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"ワープ","subitem_subject_scheme":"Other"},{"subitem_subject":"自然層流翼設計","subitem_subject_scheme":"Other"},{"subitem_subject":"NLF 翼","subitem_subject_scheme":"Other"},{"subitem_subject":"層流領域","subitem_subject_scheme":"Other"},{"subitem_subject":"空力形状","subitem_subject_scheme":"Other"},{"subitem_subject":"小型超音速実験機","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速抵抗","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer transition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cross flow instability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD inverse method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"warp","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"natural laminar flow wing design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NLF wing design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laminar region","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"scaled supersonic experimental airplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic drag","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":"航技研小型超音速実験機における自然層流翼設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航技研小型超音速実験機における自然層流翼設計"}]},"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":"37405","relation_version_is_last":true,"title":["航技研小型超音速実験機における自然層流翼設計"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:19:46.560217+00:00"}