{"created":"2023-06-20T15:08:23.409913+00:00","id":37826,"links":{},"metadata":{"_buckets":{"deposit":"e3184cca-9947-4dda-872e-5f0febbed08c"},"_deposit":{"created_by":1,"id":"37826","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37826"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037826","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["430494","430497","430496","430498","430493","430495"],"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 nonequilibrium flow around the OREX"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"22","bibliographicPageStart":"19","bibliographicVolumeNumber":"26","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_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"極超音速熱的･化学的非平衡流の解析のため新しく開発した流速ベクトル分割法を、今春成功裡に打ち上げられた軌道再突入実験機(OREX)のまわりの流れのシミュレーションに適用した。この手法は、従属変数のベクトルと時間微分のベクトルとの間の置き換えにより陰解法にもなれば陽解法にもなる。本論文では手法の導出を説明し、つぎにOREXのまわりの流れの問題に関する予備的計算結果を示す。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A flux-vector splitting scheme newly derived by the authors for analyses of hypersonic thermochemical nonequilibrium flow is applied for simulating the flow around the Orbital Reentry Experiment (OREX), which was launched in this spring successfully. The present scheme can be used for the implicit calculations as well as the explicit calculation only by replacing the vector of unknown variables into the vector of the time derivatives. In this paper the derivation of the present scheme is explained, and the calculated results of the flow problem around the OREX are also shown preliminary.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004173002","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-26","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":"東北大学 大学院"},{"subitem_text_value":"東北大学 工学部 機械航空工学科"},{"subitem_text_value":"東北大学 工学部 機械航空工学科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tohoku University Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University Department of Aeronautic and Space Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University Department of Aeronautic and Space Engineering, Faculty of Engineering"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"長友, 英夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 悟"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大宮司, 久明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagatomo, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Satoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Daiguji, Hisaaki","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":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0026002.pdf","filesize":[{"value":"342.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0026002.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37826/files/nalsp0026002.pdf"},"version_id":"64467fcb-d1c7-4a47-a810-c1b962983f2a"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"非平衡流","subitem_subject_scheme":"Other"},{"subitem_subject":"実在気体効果","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD解析","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ･ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD対風洞相関","subitem_subject_scheme":"Other"},{"subitem_subject":"OREX","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道再突入実験","subitem_subject_scheme":"Other"},{"subitem_subject":"高効率計算スキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"流束分割法","subitem_subject_scheme":"Other"},{"subitem_subject":"収束加速法","subitem_subject_scheme":"Other"},{"subitem_subject":"化学反応モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nonequilibrium flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"real gas effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equations","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD wind tunnel correlation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"OREX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbital reentry experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high efficiency numerical scheme","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flux splitting method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"convergence acceleration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"chemical reaction model","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":"OREXまわりの非平衡流れの数値計算","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"OREXまわりの非平衡流れの数値計算"}]},"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":"37826","relation_version_is_last":true,"title":["OREXまわりの非平衡流れの数値計算"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:48:47.450907+00:00"}