{"created":"2023-06-20T15:07:58.010843+00:00","id":37344,"links":{},"metadata":{"_buckets":{"deposit":"461caf9f-fe33-4057-9d2d-710bab157af6"},"_deposit":{"created_by":1,"id":"37344","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37344"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037344","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480257","480255","480256","480254"],"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 HSCT wind tunnel test model, phase 1"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"208","bibliographicPageStart":"203","bibliographicVolumeNumber":"41","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 24-26 Jun. 1998 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 24-26 Jun. 1998 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"HSCT(高速民間輸送機)空力設計用のCFD(数値流体力学)ツールを実証するために、HSCT-F1/P1標準模型のナビエ・ストークス解析を実行した。格子システムの位相は単一構造化したC-Oタイプの構造格子である。MUSCL(Monotone Upwind Schemes for Conservation Laws)法を備えたRoeの流束差分離法を空間を離散的にするために使用した。時間積分には、LU-ADI(Lower-Upper Alternating Direction Implicit)陰解法を採用した。乱流モデルはBaldwin-Lomaxの代数的モデルである。数値結果を風洞試験の結果と比較した。力データおよび圧力分布は両方ともよい一致を示したが、上面前縁において負圧ピークの不一致が見つかった。これを研究するために、工作許容精度を含むモデルや異なる迎角の場合に関して解析を行った。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Navier-Stokes analysis of HSCT (High Speed Civil Transport) F1, P1 standard model was carried out in order to validate CFD (Computational Fluid Dynamics) tool for HSCT aerodynamics design. The topology of grid system is the single structured C-O type. Roe's flux difference splitting with MUSCL (Monotone Upwind Schemes for Conservation Laws) is used to enable discrete representation of the space. LU-ADI (Lower-Upper Alternating Direction Implicit) method is adopted in time integration. The turbulence model is the algebraic model of Baldwin-Lomax. The numerical results are compared with those of wind tunnel test. Though both of forces and pressure distribution give the good agreement, the discrepancy of suction peak at upper leading edge is found. In order to investigate this, the model including the fabrication tolerance and the case with another angle of attack are analyzed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001958030","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-41","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"},{"subitem_text_value":"三菱重工業"}]},"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"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"海田, 武司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡邉, 直樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kaiden, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Naoki","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":"nalsp0041030.pdf","filesize":[{"value":"611.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0041030.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37344/files/nalsp0041030.pdf"},"version_id":"ee5d7d55-08fe-4b81-8b9e-9bd289e230e6"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HSCT","subitem_subject_scheme":"Other"},{"subitem_subject":"高速民間輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス解析","subitem_subject_scheme":"Other"},{"subitem_subject":"MUSCL","subitem_subject_scheme":"Other"},{"subitem_subject":"流束差分離法","subitem_subject_scheme":"Other"},{"subitem_subject":"LU-ADI陰解法","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"負圧ピーク","subitem_subject_scheme":"Other"},{"subitem_subject":"単純風上保存則スキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"上下交互方向陰的差分法","subitem_subject_scheme":"Other"},{"subitem_subject":"HSCT","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high speed civil transport","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":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"MUSCL","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flux difference splitting","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"LU ADI method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"suction peak","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"monotone upwind scheme for conservation law","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lower upper alternating direction implicit method","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":"HSCT模型の数値解析　その1","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HSCT模型の数値解析　その1"}]},"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":"37344","relation_version_is_last":true,"title":["HSCT模型の数値解析　その1"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:21:24.257196+00:00"}