{"created":"2023-06-20T15:07:47.000538+00:00","id":37145,"links":{},"metadata":{"_buckets":{"deposit":"eac90ad1-b513-42fd-966c-79379ff08813"},"_deposit":{"created_by":1,"id":"37145","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37145"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037145","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479125","479126","479127","479124"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical analysis of three-dimensional hypersonic non-equilibrium flows around re-entry vehicles"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"126","bibliographicPageStart":"121","bibliographicVolumeNumber":"37","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 12-13 Jun. 1997 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 12-13 Jun. 1997 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"再突入機周りの熱的・化学的に非平衡な粘性流の数値解析を行った。熱的・化学的非平衡の効果を考慮に入れるため、Parkの2温度モデルおよび7化学種有限レート反応モデルを用いた。熱的・化学的非平衡影響を考慮した3次元全ナビエ・ストークス方程式を、MUSCL(保存則に対する単調上流中心スキーム)法を用いたAUSMDV(流速差分分離および流速ベクトル分離移流上流分割法)スキームで解いた。時間積分に関して、局所時間スッテピッング法によるLU-SGS(上下対称ガウス・ザイデル)陰解法を用いて、計算時間を抑え、コード安定性を増加させた。HYFLEX(極超音速飛行実験)機の前胴部周りの数値解析を行った。圧力分布および熱流束分布を示した。リフレクトメータの前方における電子数密度分布も示した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Numerical analyzes of thermally and chemically nonequiblium viscous flow around reentry vehicles are carried out. Park's two-temperature model and seven species and finite-rate chemical reaction model are used in order to take accounts of thermal and chemical nonequilibrium effects. Three-dimensional full Navier-Stokes equations considering thermal and chemical nonequilibrium effects are solved by the AUSMDV (Advection Upstream Splitting Method DV) scheme with MUSCL (Monotone Upstream-centered Scheme for Conservation Laws) approach. Regarding time integration, the LU-SGS (Lower-Upper Symmetric Gauss-Seidel) implicit method with local time stepping method is used to suppress calculation time and increase code stability. Numerical analyzes around the fore body of HYFLEX are performed. Pressure distributions and heat flux distributions are presented. It is also presented the distribution of the number density in front of the reflectmeter.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001433019","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-37","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":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_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":"高木, 亮治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 行光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takaki, Ryoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Yukimitsu","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":"nalsp0037019.pdf","filesize":[{"value":"933.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0037019.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37145/files/nalsp0037019.pdf"},"version_id":"631d61bf-f083-4c5d-9657-deaa308c3a72"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HYFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速飛行実験","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入","subitem_subject_scheme":"Other"},{"subitem_subject":"熱的・化学的非平衡粘性流","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":"2温度モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"化学反応モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"前胴圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"熱流束分布","subitem_subject_scheme":"Other"},{"subitem_subject":"リフレクトメータ","subitem_subject_scheme":"Other"},{"subitem_subject":"電子数密度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱率","subitem_subject_scheme":"Other"},{"subitem_subject":"化学種","subitem_subject_scheme":"Other"},{"subitem_subject":"運動量保存式","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hypersonic Flight Experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermally and chemically nonequilibrium viscous flow","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":"two temperature model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"chemical reaction model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"forebody pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"heat flux distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reflectmeter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electron number density distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating rate","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"species","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"momentum conservation equation","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":"再突入物体まわりの三次元極超音速非平衡流れの解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"再突入物体まわりの三次元極超音速非平衡流れの解析"}]},"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":"37145","relation_version_is_last":true,"title":["再突入物体まわりの三次元極超音速非平衡流れの解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:24:57.668065+00:00"}