{"created":"2023-06-20T14:37:13.666261+00:00","id":3630,"links":{},"metadata":{"_buckets":{"deposit":"d036864c-694c-4cff-bd24-fd7b80211864"},"_deposit":{"created_by":1,"id":"3630","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"3630"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00003630","sets":["1398:1530:1534","1543:1874:1878","1887:1891","9:789:832:1984"]},"author_link":["14581","14578","14583","14585","14579","14580","14582","14584"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Consideration for Optimization of Fuel Distribution in a Scramjet Engine: Search by means of Tracing back along Streamlines"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2016-03-08","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"46","bibliographicPageStart":"41","bibliographicVolumeNumber":"JAXA-SP-15-013","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the 47th Fluid Dynamics Conference / the 33rd Aerospace Numerical Simulation 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":"第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム (2015年7月2日-3日. 東京大学生産技術研究所), 目黒区, 東京","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":"47th Fluid Dynamics Conference /the 33rd Aerospace Numerical Simulation Symposium (July 2-3, 2015. Institute of Industrial Science , the University of Tokyo), Meguro, Tokyo, Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Japan Aerospace Exploration Agency (JAXA) has been investigating scramjet engines in Kakuda Space Center using RamJet Engine Test Facility (RJTF) et al. The engine tested at the flight condition of Mach 6 showed very steep fuel distribution. The authors are researching the influence of cowl shock wave on the fuel distribution by using CFD based on RJTF tests, and have found advantages of strut in the engine. Here describe the authors the result of virtual experiments for optimization trial of fuel distribution in the engine by means of tracing back along streamlines in the view point where to set the fuel injection points in order to let the fuel go into high mass flux area in the engine.","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"}]},"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"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1630005005","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: JAXA-SP-15-013","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(JAXA)"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","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(JAXA)(KSPC)"},{"subitem_text_value":"スペースサービス"},{"subitem_text_value":"日立ソリューションズ東日本"},{"subitem_text_value":"日立ソリューションズ東日本"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kakuda Space Center, Japan Aerospace Exploration Agency (JAXA)(KSPC)"},{"subitem_text_language":"en","subitem_text_value":"Space Service"},{"subitem_text_language":"en","subitem_text_value":"Hitachi Solutions East Japan"},{"subitem_text_language":"en","subitem_text_value":"Hitachi Solutions East Japan"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"佐藤, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"福井, 正明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡邉, 孝宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宗像, 利彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fukui, Masaaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Takahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Munakata, Toshihiko","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":"2020-01-15"}],"displaytype":"detail","filename":"AA1630005005.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1630005005.pdf","url":"https://jaxa.repo.nii.ac.jp/record/3630/files/AA1630005005.pdf"},"version_id":"e9117fb4-817a-47cb-8093-18ba7b67e406"}]},"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":"スクラムジェットエンジン燃料最適化分布に向けた検討: 流線溯上法による探索","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"スクラムジェットエンジン燃料最適化分布に向けた検討: 流線溯上法による探索"}]},"item_type_id":"5","owner":"1","path":["1534","1878","1891","1984"],"pubdate":{"attribute_name":"公開日","attribute_value":"2016-04-21"},"publish_date":"2016-04-21","publish_status":"0","recid":"3630","relation_version_is_last":true,"title":["スクラムジェットエンジン燃料最適化分布に向けた検討: 流線溯上法による探索"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:58:06.736956+00:00"}