{"created":"2023-06-20T15:08:23.834026+00:00","id":37835,"links":{},"metadata":{"_buckets":{"deposit":"84a4cf53-4065-4045-8aea-acd6271f6b06"},"_deposit":{"created_by":1,"id":"37835","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37835"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037835","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["430534","430533","430527","430529","430528","430532","430531","430530"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical calculation of non-equilibrium flow around two-dimensional axisymmetric OREX"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"70","bibliographicPageStart":"67","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":"非平衡層流であるOREXのまわりの2次元軸対称極超音速流を数値的に計算した。強い衝撃波を含む極超音速流を安定に解くために、Roeの流束差分分割法に基く風上差分解法を採用した。気体の解離･再結合を取り扱うためParkの5種モデルを利用した。計算結果は、強い衝撃波の下流側における非平衡現象を明瞭に示す。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A two dimensional axisymmetric hypersonic flow around Orbital Reentry Experiment (OREX), that consist of non-equilibrium laminar flow, was solved numerically. Roe's flux difference splitting upwind technique was adopted to solve the hypersonic flow that contains strong shock stably. To treat dissociating-recombinating gas phenomena, Park's five-species model was utilized. The numerical result shows non-equilibrium gas phenomena behind the strong shock clearly.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004173011","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":"富士重工"},{"subitem_text_value":"スバル研究所"},{"subitem_text_value":"富士重工"},{"subitem_text_value":"富士重工"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Subaru Research Center Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Co Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"松本, 崇"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山内, 豊誠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"越岡, 康弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清島, 哲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsumoto, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamauchi, Toyosei","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koshioka, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kiyoshima, Satosi","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":"nalsp0026011.pdf","filesize":[{"value":"280.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0026011.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37835/files/nalsp0026011.pdf"},"version_id":"da7848f5-3555-4055-84bb-741b32e084dd"}]},"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":"化学的非平衡流","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":"OREX","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道再突入実験","subitem_subject_scheme":"Other"},{"subitem_subject":"数値不安定","subitem_subject_scheme":"Other"},{"subitem_subject":"カーバンクル現象","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入実験機","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙往還機","subitem_subject_scheme":"Other"},{"subitem_subject":"物体の周りの流れ","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":"chemically 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":"OREX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"orbital reentry experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical instability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"carbuncle phenomenon","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"return test vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry test vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow around body","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 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