{"created":"2023-06-20T15:07:49.039139+00:00","id":37179,"links":{},"metadata":{"_buckets":{"deposit":"3b421f4c-cdd9-4484-a5be-1cc655bd4652"},"_deposit":{"created_by":1,"id":"37179","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37179"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037179","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479341","479338","479336","479339","479337","479342","479340","479343"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A new transonic airfoil design method"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"330","bibliographicPageStart":"325","bibliographicVolumeNumber":"37","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 12-13 Jun. 1997 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 12-13 Jun. 1997 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"遷音速高揚力条件での性能向上のため、新しい翼型設計法を開発した。本手法の主概念は、衝撃波横断圧力差と境界層剥離限界との相関に基づいている。また、逆解法を組込んで設計圧力分布を実現した。本手法を用いて、遷音速高揚力性能を実現する遷音速輸送機翼の翼型を設計した。本報告では、新しい遷音速法3次元翼設計により設計された翼型の適用を試みた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A new airfoil design method was developed to improve the performance at transonic high lift condition. The main concept of the method is based on the relation between pressure difference across the shock wave and criteria for boundary-layer separation, and an inverse method is also incorporated to realize the designed pressure distribution. An airfoil was designed using this method for transonic transport wing to realize the transonic high lift performance. In this report the application of new airfoil designed here using new transonic method 3-D wing design was conducted.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001433053","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-37","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":"富士重工業"},{"subitem_text_value":"富士重工業"},{"subitem_text_value":"日本航空機開発協会"},{"subitem_text_value":"日本航空機開発協会"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Japan Aircraft Development Corporation"},{"subitem_text_language":"en","subitem_text_value":"Japan Aircraft Development Corporation"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小林, 修"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷, 泰寛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"天野, 完一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"平原, 誠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kobayashi, Osamu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tani, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Amano, Kanichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hirahara, Makoto","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":"nalsp0037053.pdf","filesize":[{"value":"568.5 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0037053.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37179/files/nalsp0037053.pdf"},"version_id":"687a0422-a904-4e11-baa2-f15dccedb41f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"翼型設計法","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"高揚力翼型","subitem_subject_scheme":"Other"},{"subitem_subject":"3次元遷音速翼","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波横断圧力差","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層剥離限界","subitem_subject_scheme":"Other"},{"subitem_subject":"オフデザイン","subitem_subject_scheme":"Other"},{"subitem_subject":"揚力係数","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速翼型逆設計法","subitem_subject_scheme":"Other"},{"subitem_subject":"揚力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"誘導抵抗","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波強さ","subitem_subject_scheme":"Other"},{"subitem_subject":"バフェット限界","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"airfoil design method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high lift airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three dimensional transonic airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure difference across shock wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer separation criteria","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"off design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lift coefficient","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic airfoil inverse design method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lift distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"induced drag","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave strength","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"buffeting criteria","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","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":"新しい遷音速翼型設計法","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"新しい遷音速翼型設計法"}]},"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":"37179","relation_version_is_last":true,"title":["新しい遷音速翼型設計法"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:24:04.015650+00:00"}