{"created":"2023-06-20T15:15:06.172879+00:00","id":45155,"links":{},"metadata":{"_buckets":{"deposit":"052598fa-27ed-4657-8dd1-b3afb75311ee"},"_deposit":{"created_by":1,"id":"45155","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45155"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045155","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["473171","473174","473173","473172","473176","473175"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1986-05","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"13","bibliographicVolumeNumber":"896T","bibliographic_titles":[{},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-896T","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"翼胴結合体まわり非粘性圧縮遷音速流をEuler方程式に基づいて数値解析するための計算法を提示する。結合体表面や無限遠等における境界条件を正確に取り入れるために結合体外部を計算空間の直方体内部に写像し,そこで一様格子を形成する。Euler方程式は二次精度のRunge-Kutta時間積分スキームと局所時間刻み技法を組入れた有限容積法によって解かれる。この計算法の有効性は三つの計算例によって実証される。得られた結果は,風洞試験の結果やコードYOKUDO-Pによる完全ポテンシャル流の解析結果と比較検討される。なお,本論文は航空宇宙技術研究所報告TR-896を要約したものである。但し,計算結果の比較にはTR-881の完全ポテンシャル流解析による結果が付記される。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A numerical procedure based on the Euler equations for analyzing the compressible inviscid transonic flow about a wing-fuselage combination is presented in this paper. In order to treat precisely boundary conditions on the combinational surface and at infinity, the exterior of the wing-fuselage combination in physical space is mapped into a rectangular parallelepiped in a computational space and then a uniform grid is generated there. The Euler equations are solved by the finite volume method using the Runge-Kutta type scheme of the second order accuracy and the local time step technique. Three examples are presented to show the utility of the numerical procedure. Numerical results obtained by the procedure are compared with experimental results and numerical results by the NAL utility code YOKUDO-P based on the full potential equation, and it is shown that the obtained results are in good agreement with the experimental data.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0896T000","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 TR-896T","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":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"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計算センター"},{"subitem_text_value":"航空宇宙技術研究所計算センター"},{"subitem_text_value":"航空宇宙技術研究所計算センター"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Computer Center, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Computer Center, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Computer Center, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"石黒, 登美子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小川, 哲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小口, 慶子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ISHIGURO, Tomiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OGAWA, Satoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OGUCHI, Keiko","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr0896t.pdf","filesize":[{"value":"896.5 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0896t.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45155/files/naltr0896t.pdf"},"version_id":"1d69e890-74a5-49c1-8380-24c50c0acf32"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"Numerical Analysis of Inviscid Compressible Flows about Wing-Fuselage Combinations based on the Euler Equations","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Numerical Analysis of Inviscid Compressible Flows about Wing-Fuselage Combinations based on the Euler Equations","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"45155","relation_version_is_last":true,"title":["Numerical Analysis of Inviscid Compressible Flows about Wing-Fuselage Combinations based on the Euler Equations"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:44:22.276353+00:00"}