{"created":"2023-06-20T15:08:23.691069+00:00","id":37832,"links":{},"metadata":{"_buckets":{"deposit":"14d5e046-224e-4209-ac98-9d943178e070"},"_deposit":{"created_by":1,"id":"37832","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37832"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037832","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["430518","430517","430520","430519"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"VSL analysis of a thermochemical nonequilibrium flow around the OREX using a three-temperature model"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"55","bibliographicPageStart":"50","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":"3温度モデルを用いた熱的･化学的非平衡流れ解析のための粘性衝撃層解法を示した。3温度モデルでは、並進と回転の温度、振動温度および電子温度をそれぞれ別々に扱う。OREXのまわりの熱的･化学的非平衡流れの解析を高度62kmにおける再突入条件の下に行った。結果は、振動と電子とのエネルギーモードの間に極めて強い結合があり、仮定した条件の下では、この2つのエネルギーモードはほとんど熱的平衡にあることを示す。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A Viscous Shock-Layer (VSL) method for thermochemical nonequilibrium flows using a three-temperature model is presented. In the three-temperature model, translational-rotational, vibrational and electron temperatures are treated separately. The analysis of a thermochemical nonequilibrium flow around the Orbital Reentry Experiment (OREX) model is performed for reentry conditions at an altitude of 62 km. The results show that there is a very strong coupling between the vibrational and the electron energy modes and the two energy modes are almost at a state of thermal equilibrium under the present conditions.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004173008","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":"富山県立大学 工学部 機械システム工学科"},{"subitem_text_value":"九州大学 工学部 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":"Toyama Prefectural University Department of Mechanical Systems Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Kyushu University Department of Aeronautics and Astronautics, Faculty of Engineering"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"坂村, 芳孝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西田, 迪雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakamura, Yoshitaka","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishida, Michio","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":"nalsp0026008.pdf","filesize":[{"value":"506.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0026008.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37832/files/nalsp0026008.pdf"},"version_id":"2163ac4c-e86e-4416-b96b-d4a4d3eb0f71"}]},"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":"OREX","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道再突入実験","subitem_subject_scheme":"Other"},{"subitem_subject":"3温度モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"粘性衝撃層解析","subitem_subject_scheme":"Other"},{"subitem_subject":"エネルギー交換モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"エネルギーモード結合","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙往還機","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入実験機","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":"OREX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbital reentry experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three temperature model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"viscous shock layer analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"energy exchange model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"energy mode coupling","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"return test vehicle","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":"3温度モデルを用いたOREX実験機周りの熱化学的非平衡流のVSL解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"3温度モデルを用いたOREX実験機周りの熱化学的非平衡流のVSL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":"37832","relation_version_is_last":true,"title":["3温度モデルを用いたOREX実験機周りの熱化学的非平衡流のVSL解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:48:37.315670+00:00"}