{"created":"2023-06-20T14:48:46.280333+00:00","id":16613,"links":{},"metadata":{"_buckets":{"deposit":"89231c3b-dac7-4ca2-b20e-81418dbf10dd"},"_deposit":{"created_by":1,"id":"16613","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"16613"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00016613","sets":["1543:1693:1703","1887:1891"]},"author_link":["151019","151018","151017","151016","151020","151015"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"One-Dimensional Simulation of Combustor Flow-field under Ramjet-Mode Operation"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2010-01","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"平成21年度","bibliographic_titles":[{"bibliographic_title":"宇宙輸送シンポジウム: 講演集録"},{"bibliographic_title":"Proceedings of Space Transportation Symposium","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":"平成21年度宇宙輸送シンポジウム(2010年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部)","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":"Space Transportation Symposium (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)),  Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A modification of the one-dimensional simulation was carried out to simulate pressure recovery due to pseudo-shock-wave system in a rocket-based combined cycle engine's combustor under dual-mode operation. So-called two flow-tubes model was employed to express the pseudo-shock-wave system observed in the engine tests. The rocket exhaust plume at a very reduced output experienced a pressure recovery to the airflow pressure, decelerated to subsonic speed. This decelerated flow was named as the low-speed flow in the two flow-tubes model. The high-speed airflow decelerated by its own while a linear portion of it was entrained into the low-speed flow, until the whole high-speed flow was entrained at the secondary fuel injector location. The modified simulation could express the gradual pressure recovery associated with the pseudo-shock-wave system, however, the resulting pressure level was higher than the measurement. The incomplete mixing in the experiment ought to the discrepancy.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"},{"subitem_description":"形態: CD-ROM1枚","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"},{"subitem_description":"Note: One CD-ROM","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064741043","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10324301","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構角田宇宙センター"},{"subitem_text_value":"宇宙航空研究開発機構角田宇宙センター"},{"subitem_text_value":"宇宙航空研究開発機構角田宇宙センター"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kakuta Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)"},{"subitem_text_language":"en","subitem_text_value":"Kakuta Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)"},{"subitem_text_language":"en","subitem_text_value":"Kakuta Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"富岡, 定毅"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"齋藤, 俊仁"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷, 香一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tomioka, Sadatake","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Toshihito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tani, Koichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Propulsion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Engines","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Combined cycle engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Performance prediction","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":"Dual-mode作動時の燃焼器内流れ場の一次元模擬について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Dual-mode作動時の燃焼器内流れ場の一次元模擬について"}]},"item_type_id":"5","owner":"1","path":["1703","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"16613","relation_version_is_last":true,"title":["Dual-mode作動時の燃焼器内流れ場の一次元模擬について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:50:17.109796+00:00"}