{"created":"2023-06-20T15:07:46.391943+00:00","id":37136,"links":{},"metadata":{"_buckets":{"deposit":"fbd650b8-1b8d-491f-a3ef-6ba79b8697a9"},"_deposit":{"created_by":1,"id":"37136","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37136"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037136","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479078","479081","479080","479079"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical analysis of supersonic transport's leading-edge vortex flaps"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"68","bibliographicPageStart":"63","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":"前縁ボルテックスフラップは、フラップ上に前縁渦を形成することにより翼の揚抗比を改善する高揚力装置の1種である。第1報では、3次元ナビエ・ストークス計算を実施し、前縁ボルテックスフラップを装備した超音速輸送クランクドアロー翼の周りの流れ場を明らかにした。今回は、風洞試験と3次元ナビエ・ストークス計算とを比較した。そして、本計算は前縁ボルテックスフラップ周りの流れ場の定量的傾向を捕えることができることを確認した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The leading-edge vortex flap is a kind of high lift device to improve the lift to drag ratio of the wing by forming a leading-edge vortex on the flap. At the 1st report, the three dimensional (3-D) Navier-Stokes calculation was carried out to clarify the flow field around the supersonic transport cranked arrow wing equipped with leading-edge vortex flaps. This time, the comparison of a wind tunnel test and the 3-D Navier-Stokes calculation were carried out. And it was confirmed that the calculation can catch the qualitative trend of the flow field around the leading-edge vortex flap.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001433010","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":"川崎重工業"}]},"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":"Kawasaki Heavy Industries Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"檜垣, 郷子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"前川, 昭二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Higaki, Kyoko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Maekawa, Shoji","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":"nalsp0037010.pdf","filesize":[{"value":"3.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0037010.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37136/files/nalsp0037010.pdf"},"version_id":"25a54fe3-6f9d-4c76-a26a-de48f072ff1f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"前縁ボルテックスフラップ","subitem_subject_scheme":"Other"},{"subitem_subject":"高揚力装置","subitem_subject_scheme":"Other"},{"subitem_subject":"揚抗比","subitem_subject_scheme":"Other"},{"subitem_subject":"3次元ナビエ・ストークス計算","subitem_subject_scheme":"Other"},{"subitem_subject":"クランクドアロー翼","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ場数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"前縁剥離渦","subitem_subject_scheme":"Other"},{"subitem_subject":"舵角","subitem_subject_scheme":"Other"},{"subitem_subject":"迎え角","subitem_subject_scheme":"Other"},{"subitem_subject":"計算格子","subitem_subject_scheme":"Other"},{"subitem_subject":"総圧分布","subitem_subject_scheme":"Other"},{"subitem_subject":"leading edge vortex flap","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high lift device","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lift to drag ratio","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three dimensional Navier Stokes calculation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"crancked arrow wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow field numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"leading edge separation vortex","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flap angle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attack angle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"calculation grid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"total pressure distribution","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":"超音速輸送機の前縁ボルテックス・フラップ周りの流れの数値解析　第2報","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速輸送機の前縁ボルテックス・フラップ周りの流れの数値解析　第2報"}]},"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":"37136","relation_version_is_last":true,"title":["超音速輸送機の前縁ボルテックス・フラップ周りの流れの数値解析　第2報"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:25:10.731778+00:00"}