{"created":"2023-06-20T15:13:17.516893+00:00","id":43217,"links":{},"metadata":{"_buckets":{"deposit":"14729015-1b28-446a-beee-aa9aaf70bf72"},"_deposit":{"created_by":1,"id":"43217","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43217"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043217","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462659","462658","462657","462656"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"An Analysis of the Compressible-Viscous Flow Field Around a 3D-Oscillating Wing"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1986-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"12","bibliographicPageStart":"1","bibliographicVolumeNumber":"7","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 SP-7","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A 3D Navier-Stokes program based upon a Beam-Warming diagonalization scheme has been combined with a moving grid system so that it can be applied to the solution around an oscillating wing. The wing is in a pitching motion with an amplitude of 1 degrees and a reduced frequency of 0.428 (based upon the root semichord). The free stream Mach number is 0.9 and the mean angle of attack of the wing is 4 degrees. To the extent that results have been compared with experimental data, the unsteady flow is successfully simulated and the leading edge separations are observed, which is one of the most significant aspects of the experiment. It is demonstrated that the present code is feasible and applicable to the computation of the unsteady viscous compressible flow field around an oscillating wing.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0007001","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-7","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_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_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所機体第一部"},{"subitem_text_value":"航空宇宙技術研究所機体第一部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中道, 二郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"磯貝, 紘二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamichi, Jiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Isogai, Koji","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":"2020-01-28"}],"displaytype":"detail","filename":"nalsp0007001.pdf","filesize":[{"value":"695.1 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0007001.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43217/files/nalsp0007001.pdf"},"version_id":"2f80720d-7ad5-4fa7-a1c6-8d366d7a3420"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"三次元振動翼回りの圧縮粘性流解析の一試み","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"三次元振動翼回りの圧縮粘性流解析の一試み"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43217","relation_version_is_last":true,"title":["三次元振動翼回りの圧縮粘性流解析の一試み"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:20:04.626158+00:00"}