{"created":"2023-06-20T14:37:57.469978+00:00","id":4412,"links":{},"metadata":{"_buckets":{"deposit":"5150cdcb-0f08-4f0e-893e-c2410cbdc6c6"},"_deposit":{"created_by":1,"id":"4412","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"4412"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00004412","sets":["1398:1530:1538","1543:1874:1882","1887:1891","9:789:906:907"]},"author_link":["19840","19838","19839","19842","19837","19843","19836","19841"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Consideration on Defining Strut Tail Shape in a Scramjet Engine"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2012-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"236","bibliographicPageStart":"231","bibliographicVolumeNumber":"JAXA-SP-11-015","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第43回流体力学講演会: 航空宇宙数値シミュレーション技術シンポジウム2011論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011","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43回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2011 (2011年7月7日-8日. 早稲田大学国際会議場) 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":"43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8,  2011. Waseda University, International Conference Center), 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 Ram Jet Engine Test Facililty (RJTF) et al. The engine performance tested at the flight condition of Mach 6 in RJTF showed very important characteristics depending on internal geometry. The authors found in the result of CFD research that there was a hot area caused by 3-dimensional interaction of the shock wave from cowl leading edge and the shock wave from strut leading edge and that the area \"hot triagle\" contributes to intensive combustion transition.  Two engine configurations are compared to the engine configuration with 5/5 height strut that showed good thrust performance in the engine test. One is a configuration with tail-tapered strut (5/5 height) that are intended to reduce the engine inflow drag first, and the other one is a configuration with boat-tail strut (5/5 height) that has a finite width at its tail edge to produce fuel residence time in the recirculation region after itself. CFD is carried out in the case of the two configurations to solve the inner air flow, and the drag and the residence time are made clear. It is found that the configuration with boat-tail srut not only can reduce drag but also produce the finite residence time in the recirculation region.","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: AA0065207040","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-11-015","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"}]},"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 (JAXA)"},{"subitem_text_value":"日立東日本ソリューションズ"},{"subitem_text_value":"日立東日本ソリューションズ"},{"subitem_text_value":"日立東日本ソリューションズ"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Hitachi East Japan Solutions"},{"subitem_text_language":"en","subitem_text_value":"Hitachi East Japan Solutions"},{"subitem_text_language":"en","subitem_text_value":"Hitachi East Japan Solutions"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"佐藤, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡邉, 孝宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"福井, 正明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宗像, 利彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Takahiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fukui, Masaaki","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":"2020-01-16"}],"displaytype":"detail","filename":"65207040.pdf","filesize":[{"value":"670.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"65207040.pdf","url":"https://jaxa.repo.nii.ac.jp/record/4412/files/65207040.pdf"},"version_id":"a6287ef8-9364-4b41-9900-9d5e8e859961"}]},"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におけるストラット後縁形状決定法に関する検討","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におけるストラット後縁形状決定法に関する検討"}]},"item_type_id":"5","owner":"1","path":["907","1538","1882","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"4412","relation_version_is_last":true,"title":["スクラムジェットエンジンにおけるストラット後縁形状決定法に関する検討"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:39:58.240714+00:00"}