{"created":"2023-06-20T15:08:21.377926+00:00","id":37782,"links":{},"metadata":{"_buckets":{"deposit":"db48f9d4-ed81-4d92-ba9a-f321ef4a6630"},"_deposit":{"created_by":1,"id":"37782","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37782"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037782","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["482962","482960","482959","482961"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Direct simulation of fuel combustions in a supersonic shear flow"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"132","bibliographicPageStart":"127","bibliographicVolumeNumber":"22","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第11回航空機計算空気力学シンポジウム論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of the 11th NAL Symposium on aircraft computational aerodynamics","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 10-11 Jun. 1993 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 10-11 Jun. 1993 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"ボルツマン方程式に基づいた直接シミュレーションモンテカルロ法を用い、平板で仕切られた超音速空気流と音速水素気流の2つの平行な流れが平板の後端(リップ)で出会って生成する2次元超音速剪断流における燃料ガス混合と化学反応を解析した。水素ガス温度が剪断流内部の混合に及ぼす影響が明らかにされ、また、16反応系を適用することにより、混合と吸/発熱反応領域との関係が調べられ、点火過程の詳細が明らかになった。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Direct Simulation Monte Carlo (DSMC) Method based on the Boltzmann equation has been employed to analyze fuel gas mixing and reaction in two-dimensional supersonic shear flow which is formed due to the meeting at a thin plate (lip) edge of two parallel flows, a supersonic air stream and a sonic hydrogen gas flow. The influence of hydrogen gas temperature upon the mixing within shear layer has been clarified and by applying 16 reaction system the relationship between the mixing and the endo/exothermic reaction region has been analyzed to reveal the details of ignition process.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004171022","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-22","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":"東京大学 大学院"},{"subitem_text_value":"東京大学 工学部　航空宇宙工学科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"University of Tokyo Graduate School"},{"subitem_text_language":"en","subitem_text_value":"University of Tokyo Department of Aeronautics and Astronautics, Faculty of Engineering"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小幡, 茂男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"長島, 利夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Obata, Shigeo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagashima, Toshio","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":"nalsp0022021.pdf","filesize":[{"value":"518.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0022021.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37782/files/nalsp0022021.pdf"},"version_id":"c30a55e5-9d35-4223-ba64-84dcabef4247"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"燃焼過程","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速剪断流","subitem_subject_scheme":"Other"},{"subitem_subject":"DSMC","subitem_subject_scheme":"Other"},{"subitem_subject":"直接シミュレーションモンテカルロ法","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速燃焼","subitem_subject_scheme":"Other"},{"subitem_subject":"燃料燃焼","subitem_subject_scheme":"Other"},{"subitem_subject":"燃焼器内流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"空燃混合","subitem_subject_scheme":"Other"},{"subitem_subject":"混合過程","subitem_subject_scheme":"Other"},{"subitem_subject":"点火過程","subitem_subject_scheme":"Other"},{"subitem_subject":"化学反応過程","subitem_subject_scheme":"Other"},{"subitem_subject":"混合効率","subitem_subject_scheme":"Other"},{"subitem_subject":"吸発熱反応領域","subitem_subject_scheme":"Other"},{"subitem_subject":"ボルツマン方程式数値解","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"combustion process","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic shear flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"DSMC","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Direct Simulation Monte Carlo method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic combustion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fuel combustion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combustor flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fuel air mixing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mixing process","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ignition process","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"chemical reaction process","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mixing efficiency","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"endo exothermic reaction region","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Boltzmann equation solution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","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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