{"created":"2023-06-20T14:48:46.325449+00:00","id":16614,"links":{},"metadata":{"_buckets":{"deposit":"f81b9491-686b-4650-92fa-16202b78a625"},"_deposit":{"created_by":1,"id":"16614","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"16614"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00016614","sets":["1543:1693:1703","1887:1891"]},"author_link":["151026","151029","151027","151024","151021","151028","151023","151022","151025","151030"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Ramjet- / Scramjet-Mode Combustion with Supersonic Diamond-shaped Injector"}]},"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":"Supersonic injections through diamond-shaped injectors were applied to a supersonic combustor with a diverging section, with a Mach 2.4 incoming vitiated airflow at a total temperature of 2000 K, and combustion characteristics were experimentally investigated and compared to those with sonic injection through circular injectors. Without any flame-holding devices installed, scramjet-mode combustion was attained in wide range of fuel flow rate, in which the supersonic injections resulted in a higher pressure-rise in far-field than the sonic injections. Regardless of the injection scheme (i.e, orifice shape, orifice number, and injection conditions), transition to dual-mode combustion enhanced the thrust production, and the supersonic injection through the diamond-shaped orifice had lesser ability to cause the transition than the sonic injection through the circular orifice. The ability was enhanced by installation of a recess and introduction of recess fueling, and resulting combustor performance was slightly better than that with the sonic injection.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"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":"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: AA0064741044","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":"東京工業大学大学院総合理工学研究科"},{"subitem_text_value":"東京工業大学大学院総合理工学研究科"},{"subitem_text_value":"慶應義塾大学理工学部機械工学科"}]},"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":"Interdisciplinary Graduate School of Science and Engineering, Tokyo Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Interdisciplinary Graduate School of Science and Engineering, Tokyo Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical Engineering, Faculty of Science and Technology, Keio Univeristy"}]},"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":"泉川, 宗男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"増本, 量"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山岬, 裕之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松尾, 亜紀子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tomioka, Sadatake","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Izumikawa, Muneo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Masumoto, Ryo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamasaki, Hiroyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuo, Akiko","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":"Fuel Injection","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Combustion","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":"菱形孔超音速噴射器を用いたラム・スクラムモード燃焼","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"菱形孔超音速噴射器を用いたラム・スクラムモード燃焼"}]},"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":"16614","relation_version_is_last":true,"title":["菱形孔超音速噴射器を用いたラム・スクラムモード燃焼"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T04:50:16.186491+00:00"}