{"created":"2023-06-20T15:07:29.892132+00:00","id":36866,"links":{},"metadata":{"_buckets":{"deposit":"bd08f820-be48-4d36-af5f-2f7d9e026166"},"_deposit":{"created_by":1,"id":"36866","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36866"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036866","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477920","477919"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"圧縮性ナビエ・ストークス方程式解のための新規高解像度スキーム"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"38","bibliographicPageStart":"33","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":"一点静止衝撃波捕獲を生じる流束の分離および抑制の新規手法を報告した。手法を完全ナビエ・ストークスならびにレイノルズ平均化ナビエ・ストークス方程式に適用した。亜音速、超音速速度における層流境界層の計算を翼周りの遷音速流の計算と共に示した。結果は理論的解あるいは既存の実験データと非常によく一致した。提案したスキームは一点衝撃波捕獲性を維持し、かつ粘性流の解像度を向上させた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A new flux splitting and limiting technique which yields one-point stationary shock capturing is presented. The technique is applied to the full Navier-Stokes and Reynolds averaged Navier-Stokes equations. Calculations of laminar boundary layer at subsonic and supersonic speeds are presented together with calculations of transonic flows around airfoils. The results show very good agreement with theoretical solutions or existing experimental data. It is shown that the proposed scheme improves the resolution of viscous flows while maintaining one-point shock capturing property.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000685007","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":"三菱重工業 名古屋航空宇宙システム製作所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd Nagoya Aerospace Systems Works"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"巽, 重文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tatsumi, Shigefumi","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":"nalsp0034007.pdf","filesize":[{"value":"927.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0034007.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36866/files/nalsp0034007.pdf"},"version_id":"b213e7e5-a705-49a2-90fc-8b56c129a63b"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"高解像度スキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"流束分離","subitem_subject_scheme":"Other"},{"subitem_subject":"流束抑制","subitem_subject_scheme":"Other"},{"subitem_subject":"一点衝撃波捕獲","subitem_subject_scheme":"Other"},{"subitem_subject":"層流境界層","subitem_subject_scheme":"Other"},{"subitem_subject":"亜音速","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮性粘性流","subitem_subject_scheme":"Other"},{"subitem_subject":"オイラー方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"high resolution scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flux splitting","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flux limiting","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"one point shock capturing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laminar boundary layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"subsonic speed","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic speed","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressible viscous flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Euler equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"A new high resolution scheme for the solution of the compressible Navier-Stokes equations","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"A new high resolution scheme for the solution of the compressible Navier-Stokes equations","subitem_title_language":"en"}]},"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":"36866","relation_version_is_last":true,"title":["A new high resolution scheme for the solution of the compressible Navier-Stokes equations"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:30:19.488572+00:00"}