{"created":"2023-06-20T15:07:23.527388+00:00","id":36760,"links":{},"metadata":{"_buckets":{"deposit":"257b762c-1e74-4201-867e-0f0145939303"},"_deposit":{"created_by":1,"id":"36760","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36760"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036760","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477466","477467"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"OREX回りの極超音速流れ場の数値計算シミュレーション"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"127","bibliographicPageStart":"122","bibliographicVolumeNumber":"29","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 8 Jun. 1995 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 8 Jun. 1995 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"OREX(軌道再突入実験機)回りの極超音速流れ場が、三菱重工業(MHI)の極超音速ナビエ・ストークスコードCHRIS(極超音速再突入情報統合のためのコンピュータコード)でシミュレートされた。このコードは、対流項のMUSCL(保存則のための単調な上流スキーム)型のより高次の正確な公式化をもつRoeのRiemann解法を使用する風上、陰的、有限差分法を基礎にしている。実在気体効果は、平衡空気特性の単純曲線適合を持つVEG(可変等価ガンマ)を使って考慮された。OREXの計算は、平衡気体および完全気体の仮定のもとで行われた。実在気体と完全気体の計算で得られた結果の比較が討議された。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The hypersonic flowfields around the OREX (Orbital Reentry Experiment) have been simulated by the MHI (Mitsubishi Heavy Industries) hypersonic Navier-Stokes code CHRIS (Computer code for Hypersonic Reentry Information Synthesis). This code is based on the upwind, implicit, finite-difference method using Roe's Riemann solver with MUSCL (Monotonic Upstream Schemes for Conservation Laws) type higher-order accurate formulation of the convective terms. The real gas effects are taken into consideration using a VEG (Variable Equivalent Gamma) method with simplified curve fit of equilibrium air properties. Computations for the OREX are done under the assumption of equilibrium gas and perfect gas. Comparisons between the results obtained for real gas and perfect gas calculations are discussed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000110010","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-29","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"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中尾, 雅弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakao, Masahiro","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":"nalsp0029010.pdf","filesize":[{"value":"400.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0029010.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36760/files/nalsp0029010.pdf"},"version_id":"46c3b00a-a7e1-4fd0-a9ca-dddf0977c186"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速ナビエ・ストークコード","subitem_subject_scheme":"Other"},{"subitem_subject":"RoeのRiemann解法","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":"極超音速流れ場","subitem_subject_scheme":"Other"},{"subitem_subject":"CHRIS","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速再突入情報統合のためのコンピュータコード","subitem_subject_scheme":"Other"},{"subitem_subject":"MUSCL","subitem_subject_scheme":"Other"},{"subitem_subject":"保存則のための単調な上流スキーム","subitem_subject_scheme":"Other"},{"subitem_subject":"風上陰的有限差分法","subitem_subject_scheme":"Other"},{"subitem_subject":"平衡気体","subitem_subject_scheme":"Other"},{"subitem_subject":"完全気体","subitem_subject_scheme":"Other"},{"subitem_subject":"VEG","subitem_subject_scheme":"Other"},{"subitem_subject":"変化相当ガンマ","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic Navier-Stokes code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Roe's Riemann solver","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":"hypersonic flow field","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CHRIS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computer code for hypersonic reentry information synthesis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"MUSCL","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"monotonic upstream schemes for conservation law","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"finite difference method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"equilibrium gas","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"perfect gas","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"VEG","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"variable equivalent gamma","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Numerical simulations of the hypersonic flowfields around OREX","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Numerical simulations of the hypersonic flowfields around OREX","subitem_title_language":"en"}]},"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":"36760","relation_version_is_last":true,"title":["Numerical simulations of the hypersonic flowfields around OREX"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:32:16.241234+00:00"}