{"created":"2023-06-20T15:07:30.224088+00:00","id":36871,"links":{},"metadata":{"_buckets":{"deposit":"adeb0002-af48-4915-b739-2dceea66ddbb"},"_deposit":{"created_by":1,"id":"36871","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36871"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036871","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477941","477942","477940","477939","477937","477938"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Summary of high enthalpy flow workshop"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"66","bibliographicPageStart":"61","bibliographicVolumeNumber":"34","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 6-7 JUN. 1996 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 6-7 JUN. 1996 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"日本の宇宙プロジェクトを展望すると、宇宙飛行体の大気再突入の間に発生する高エンタルピー、高マッハ数流れに関する知識が最近かなりの関心を呼んできている。実験が極めて困難で費用の掛かる宇宙環境下の宇宙飛行体の空力設計を支援する必要性から、数値シミュレーションの利用が促された。このような状況から、軸対称流問題についての高エンタルピー流れワークショップを1995年6月にNALで開催した。OREX(軌道再突入実験機)実在気体流れ問題の計算結果を要約し、各数値結果の詳細な比較を論じた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In the perspective of Japanese space projects, the knowledge of high enthalpy and high Mach number flow, occurring during the atmospheric reentry of space vehicles, has regained recently considerable interest. The need to support aerodynamic design of space vehicles under the environments where experiment is very difficult and costly, has driven the use of numerical simulation. Hence, high enthalpy flow workshop was held at NAL in June, 1995 for axisymmetric flow problems. This paper summarizes the computational results of OREX (Orbital Reentry Experiment) real gas flow problem and discusses the detailed comparison of each numerical results.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000685012","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-34","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":"三向ソフトウェア開発"},{"subitem_text_value":"三向ソフトウェア開発"}]},"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":"Sanko Software Ltd"},{"subitem_text_language":"en","subitem_text_value":"Sanko Software Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山本, 行光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"保阪, 陽子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"斉藤, 亜希子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Yukimitsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hosaka, Yoko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Akiko","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":"nalsp0034012.pdf","filesize":[{"value":"607.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0034012.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36871/files/nalsp0034012.pdf"},"version_id":"794f6047-a907-4fef-acf1-6063e3b5e4ff"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"高エンタルピー流","subitem_subject_scheme":"Other"},{"subitem_subject":"高マッハ数流","subitem_subject_scheme":"Other"},{"subitem_subject":"大気再突入","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙飛行体","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"よどみ点流","subitem_subject_scheme":"Other"},{"subitem_subject":"軸対称流","subitem_subject_scheme":"Other"},{"subitem_subject":"実在気体流","subitem_subject_scheme":"Other"},{"subitem_subject":"OREX","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道再突入実験機","subitem_subject_scheme":"Other"},{"subitem_subject":"非触媒壁面","subitem_subject_scheme":"Other"},{"subitem_subject":"high enthalpy flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high Mach number flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"atmospheric reentry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stagnation point flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"axisymmetric flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"real gas flow","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":"noncatalytic surface","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":"高エンタルピー流れワークショップまとめ","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"高エンタルピー流れワークショップまとめ"}]},"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":"36871","relation_version_is_last":true,"title":["高エンタルピー流れワークショップまとめ"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:30:11.475276+00:00"}