{"created":"2023-06-20T15:07:33.079810+00:00","id":36913,"links":{},"metadata":{"_buckets":{"deposit":"e584d06a-34c2-4cf5-9913-b694ed40b6b2"},"_deposit":{"created_by":1,"id":"36913","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36913"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036913","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["478188","478185","478186","478187"],"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":"1997-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"312","bibliographicPageStart":"307","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":"超音速輸送機の主翼はしばしばデルタ翼あるいはデルタ状翼になっている。離着陸条件下ではデルタ翼あるいはデルタ状翼の揚抗比はあまりよくないことが分かっている。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して翼の揚抗比を改善することができる。前縁ボルテックス・フラップを装備した超音速輸送機クランクト・アロー翼周りの流れ場を明らかにするために3次元ナビエ・ストークス計算を行った。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The supersonic transports often have a delta or delta-like wing for the main wing. It is known that the lift to drag ratio of a delta or delta-like wing at a take-off and landing condition is not so good. The leading-edge vortex flap can improve the lift to drag ratio of the wing by forming a leading-edge vortex on the flap. The 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.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000685054","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":"富士重工業"},{"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":"Japan Aircraft Development Corporation"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"檜垣, 郷子"}],"nameIdentifiers":[{"nameIdentifier":"478185","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"前川, 昭二"}],"nameIdentifiers":[{"nameIdentifier":"478186","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Higaki, Kyoko","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"478187","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Maekawa, Shoji","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"478188","nameIdentifierScheme":"WEKO"}]}]},"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":"nalsp0034054.pdf","filesize":[{"value":"2.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0034054.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36913/files/nalsp0034054.pdf"},"version_id":"5e8badc0-37bb-43e2-89e6-277d68c283a5"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"前縁ボルテックスフラップ","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"デルタ翼","subitem_subject_scheme":"Other"},{"subitem_subject":"揚抗比","subitem_subject_scheme":"Other"},{"subitem_subject":"離陸条件","subitem_subject_scheme":"Other"},{"subitem_subject":"着陸条件","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":"流れ場","subitem_subject_scheme":"Other"},{"subitem_subject":"クランクトアロー翼","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"leading edge vortex flap","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"delta wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lift to drag ratio","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"take off condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"landing condition","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":"flow field","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"cranked arrow wing","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","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"}]},"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":"36913","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"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:29:09.712872+00:00"}