{"created":"2023-06-20T15:08:17.554092+00:00","id":37704,"links":{},"metadata":{"_buckets":{"deposit":"4518275d-e441-4c9a-b6c5-4896ab8fa4e1"},"_deposit":{"created_by":1,"id":"37704","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37704"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037704","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482591","482587","482585","482584","482590","482586","482589","482588"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Role of computational fluid dynamics in aeronautical engineering. 10: Numerical analysis of flow around 2-D multi-element HLD"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"104","bibliographicPageStart":"99","bibliographicVolumeNumber":"19","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第10回航空機計算空気力学シンポジウム論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of the NAL symposium on aircraft computational aerodynamics","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 10-12 Jun. 1992 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 10-12 Jun. 1992 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"多翼素から成る高揚力装置のまわりの流れの2次元ナビエ・ストークス解析を行った。広い迎角の範囲における空力特性を計算するためにq-ω2方程式乱流モデルを用いた。計算結果は、大迎角においてフラップの上面に剥離をもたない大規模な粘性伴流領域があることを示す。高いレイノルズ数では、レイノルズ数の増加に対して揚力係数が減少する例がみられた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"2-dimensional Navier-Stokes analysis of flow around multi-element high lift devices was carried out. In order to calculate the aerodynamic characteristics in wide range of angle of attack, q-omega 2-equations turbulence model was used. Numerical results show flowfields with large viscous wake region without flow separation on the top surface of the flap at large angle of attack. In high Reynolds number cases, numerical results of decrease in lift coefficient were computed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004168018","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-19","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":"川崎重工業 岐阜技術研究所"},{"subitem_text_value":"川崎重工業 岐阜技術研究所"},{"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":"Kawasaki Heavy Industries LTD Gifu Technical Institute"},{"subitem_text_language":"en","subitem_text_value":"Kawasaki Heavy Industries LTD Gifu Technical Institute"},{"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":"恵上, 浩一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"嶋, 英志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"天野, 完一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 槙悟"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Egami, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shima, Eiji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Amano, Kan-ichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Shingo","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":"nalsp0019018.pdf","filesize":[{"value":"555.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0019018.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37704/files/nalsp0019018.pdf"},"version_id":"85855554-5c09-4c26-8ddc-27b442661d7d"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"多翼素翼型","subitem_subject_scheme":"Other"},{"subitem_subject":"高揚力装置","subitem_subject_scheme":"Other"},{"subitem_subject":"空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"高迎角","subitem_subject_scheme":"Other"},{"subitem_subject":"翼特性","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮性粘性流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD解析","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学解析","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"2方程式乱流モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"レイノルズ数効果","subitem_subject_scheme":"Other"},{"subitem_subject":"翼型伴流特性","subitem_subject_scheme":"Other"},{"subitem_subject":"計算格子効果","subitem_subject_scheme":"Other"},{"subitem_subject":"multielement airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high lift device","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high angle of attack","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airfoil characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressible viscous flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two equation turbulence model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Reynolds number effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airfoil wake characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational grid effect","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 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