{"created":"2023-06-20T15:08:20.783399+00:00","id":37770,"links":{},"metadata":{"_buckets":{"deposit":"7d2436cd-8e7e-4ed1-a71c-cf9006f37270"},"_deposit":{"created_by":1,"id":"37770","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37770"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037770","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482899","482900"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Compendium of results: Flow analysis around ONERA model M5 configuration"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"59","bibliographicPageStart":"56","bibliographicVolumeNumber":"22","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第11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 11th 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 10-11 Jun. 1993 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 10-11 Jun. 1993 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"「3次元課題:ONERA(フランス国立航空宇宙研究所)M-5翼まわりの流れの解析」の結果報告を与えた。提出された計算結果の全ては、相互および実験データとの差をみるためそれぞれの図により示された。「課題A:一様流マッハ数0.84、迎角α=-1度、レイノルズ数1×10｛6｝で自由遷移の場合」および「課題B:一様流マッハ数0.84、迎角α=-1度、レイノルズ数6×10｛7｝で全面乱流の場合」において、圧力分布および揚力面と胴体上の等圧線とを比較した。レイノルズ数1×10｛6｝における実験データも示した。課題Aにおいて主翼上における境界層遷移線を比較した。「課題C:模型機体空力特性の計算」では、CL〜α、CL〜CD、CL〜CM曲線を実験データと比較して示した。これらの結果に導く要因および今後に必要な改良について論じた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Compendium of results of three dimensional problem; flow analysis around ONERA M5 (Office National d'Etudes et d'Recherches Aerospatiales) configuration is given. All of the submitted computation results were shown on the respective figures to see the differences between the computed results and experimental data. In Problem A; flow analysis with freestream condition of Mach number, 0.84. alpha = minus one deg, Reynolds number. 1 X 10(exp 6) with free transition condition and Problem B; flow analysis with freestream condition of Mach number, 0.84, alpha = minus one deg, Reynolds number. 6 X 10(exp 6) with fully turbulent conditions. the pressure distributions and Cp contours on the lifting surface and the fuselage were compared. Experimental data with Reynolds number 1 X 10(exp 6) were also shown. In Problem A. the computed transition lines of the main wing surface were compared. In Problem C: computation of aerodynamic characteristics of the Model aircraft, the C(sub L) - alpha, C(sub L) - C(sub D) and C(sub L) - C(sub M), curves were shown in comparison with experimental data. The factors leading to the present results were discussed and necessary future improvement were also discussed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004171010","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-22","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 構造力学部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structural Mechanics Division"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中道, 二郎"}],"nameIdentifiers":[{"nameIdentifier":"482899","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Nakamichi, Jiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"482900","nameIdentifierScheme":"WEKO"}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"CFDコード比較","subitem_subject_scheme":"Other"},{"subitem_subject":"CFDコード信頼性","subitem_subject_scheme":"Other"},{"subitem_subject":"CFDコード検証","subitem_subject_scheme":"Other"},{"subitem_subject":"CFDコード性能","subitem_subject_scheme":"Other"},{"subitem_subject":"CFDワークショップ","subitem_subject_scheme":"Other"},{"subitem_subject":"ワークショップ報告","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式数値解法","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD対風洞相関","subitem_subject_scheme":"Other"},{"subitem_subject":"ONERA　M5　全機模型","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速3次元翼流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速翼","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波特性","subitem_subject_scheme":"Other"},{"subitem_subject":"3次元翼","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層遷移位置","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD code comparison","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD code reliability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD code validation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD code performance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD workshop","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"workshop conpendium","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation solution method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD wind tunnel correlation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ONERA M5 mode","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic three dimensional wing flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three dimensional wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer transition position","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":"報告　3次元部門課題:ONERA　M5　全機形態まわり流れ解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"報告　3次元部門課題:ONERA　M5　全機形態まわり流れ解析"}]},"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":"37770","relation_version_is_last":true,"title":["報告　3次元部門課題:ONERA　M5　全機形態まわり流れ解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:12:49.887993+00:00"}