{"created":"2023-06-20T15:08:20.386872+00:00","id":37762,"links":{},"metadata":{"_buckets":{"deposit":"b1dae6d7-0894-40bf-aaff-4229625570c9"},"_deposit":{"created_by":1,"id":"37762","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37762"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037762","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482874","482872","482870","482871","482869","482873"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical simulation of transonic wind tunnel flows about a fully configured model of aircraft"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"18","bibliographicPageStart":"13","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":"数値計算法の信頼性を調べるため、航技研(NAL)遷音速風洞内のONERA(フランス国立航空宇宙研究所)M5全機模型のまわりの流れを数値的に解いている。その一環として今回は、風洞内の計算領域を拡大した場合を扱った。複雑な形状のまわりの風洞内流れの計算を実行するため複合格子法を用い、また、遷音速風洞多孔壁を通過する流れについてモデル化を行った。静圧分布、揚力および抗力の計算値が実験値とよく一致したことから、この試みは成功したといえる。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A series of trials to numerically analyze NAL transonic wind-tunnel flows about a fully configured model of aircraft, ONERA-M5 (Office National d'Etudes et d'Recherches Aerospatiales), has been performed to investigate the reliability of numerical computations, and in this time the computational region within the wind tunnel has been enlarged. To realize computations of wind-tunnel flows about a complicated configuration, a multi-domain technique and a model of outflow through the perforated wall of the transonic wind-tunnel are used. As a result it is known that this trial is successful since the computed pressure, lift and drag coefficients agree well with experimental ones.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004171002","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":"富士通"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"FUJITSU LIMITED"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory ogy"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"高倉, 葉子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小川, 哲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"和田, 安弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takakura, Yoko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ogawa, Satoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wada, Yasuhiro","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":"nalsp0022002.pdf","filesize":[{"value":"624.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0022002.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37762/files/nalsp0022002.pdf"},"version_id":"fadf7ae6-21db-4d9e-b0ce-0011f143a407"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"風洞内流れシミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"ONERA　M5翼模型","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式数値解","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"多孔壁境界条件","subitem_subject_scheme":"Other"},{"subitem_subject":"模型支持干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"複合格子法","subitem_subject_scheme":"Other"},{"subitem_subject":"複合格子形成","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速3重衝撃波","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速3次元翼","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ONERA M5 wing model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation numerical solution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"perforated wall boundary condition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"model support interference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiple domain technique","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiple domain grid generation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic triple shock wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic three dimensional wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Computational Fluid Dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","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":"遷音速風洞内全機模型流れの数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"遷音速風洞内全機模型流れの数値シミュレーション"}]},"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":"37762","relation_version_is_last":true,"title":["遷音速風洞内全機模型流れの数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:13:02.059791+00:00"}