{"created":"2023-06-20T15:07:43.695979+00:00","id":37095,"links":{},"metadata":{"_buckets":{"deposit":"04ce65a8-aff9-4a82-8281-8f28f5e6cb1a"},"_deposit":{"created_by":1,"id":"37095","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37095"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037095","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["478900","478905","478904","478902","478903","478901"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Experiments on supersonic turbulent mixing and combustion using streamwise vorticity generating type fuel injectors"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"20","bibliographicPageStart":"17","bibliographicVolumeNumber":"36","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","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 26-28 Mar. 1997 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 26-28 Mar. 1997 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"縦渦導入型燃料噴射器を用いてマッハ2.5主流中の超音速混合および燃焼を試験した。噴射器のひとつは「AW(Alternating Wedge)ストラット」で、スパン方向に並んだ互いに逆回転する4組の縦渦を導入することが可能である。他の噴射器は「S(スウェプト)ランプ噴射器」で、互いに逆回転する1対の縦渦を導入することが可能である。燃焼を伴う流れの中の縦渦形成過程は非燃焼時流内でAWストラットを使用した場合の渦形成過程にほぼ類似していた。AWストラットおよびSランプ噴射器を従来型の壁面噴射器やストラット型噴射器と比較した。ダクト出口における壁面圧力分布と局所当量比の測定結果は、他の従来型壁面有角噴射器やストラット型噴射器の利用と比較して、縦渦の利用により混合と燃焼が著しく増進することを示した。非燃焼流中で検討した縦渦を用いた混合制御手法を実際の燃焼時の混合・燃焼増強に適用することは可能であり有効である。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Supersonic mixing and combustion were examined using streamwise vorticity generating type fuel injectors in a Mach 2.5 freestream. One of such injectors was 'Alternating Wedge (A.W.) strut' which could introduce four pair of counter-rotating streamwise vortices in spanwise row configuration. Another injector was 'swept ramp' injector which could introduce a pair of counter-rotating streamwise vortices. The process of streamwise vortex development in the flow with combustion were almost similar to that in the cold flow in the case of A.W. strut. A.W. strut and swept ramp injectors were compared with some traditional wall-injectors and strut-injectors. The wall pressure distributions and the local equivalence ratios at the exit of the duct showed that the mixing and the combustion were highly enhanced by the use of streamwise vortices compared with the use of other traditional wall-injectors and strut-injectors. It is possible and effective to apply the mixing control technique using streamwise vortices studied in the cold flow to the mixing and combustion enhancement in a real combustor.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001320005","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-36","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":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"大阪府立大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"Osaka Prefecture University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"須浪, 徹治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wendt, Michael N."}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西岡, 通男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sunami, Tetsuji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wendt, Michael N.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishioka, Michio","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":"nalsp0036005.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0036005.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37095/files/nalsp0036005.pdf"},"version_id":"25740bf1-35a6-45e8-be7e-b2d7bae9e2f3"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速乱流混合","subitem_subject_scheme":"Other"},{"subitem_subject":"縦渦導入型","subitem_subject_scheme":"Other"},{"subitem_subject":"燃料噴射器","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速燃焼","subitem_subject_scheme":"Other"},{"subitem_subject":"AWストラット噴射器","subitem_subject_scheme":"Other"},{"subitem_subject":"交互くさび型ストラット噴射器","subitem_subject_scheme":"Other"},{"subitem_subject":"Sランプ噴射器","subitem_subject_scheme":"Other"},{"subitem_subject":"スウェプトランプ噴射器","subitem_subject_scheme":"Other"},{"subitem_subject":"反対方向回転渦","subitem_subject_scheme":"Other"},{"subitem_subject":"渦形成過程","subitem_subject_scheme":"Other"},{"subitem_subject":"壁面有角噴射器","subitem_subject_scheme":"Other"},{"subitem_subject":"壁面圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"局所当量比","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic turbulent mixing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"streamwise vorticity generating type","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fuel injector","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic combustion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"AW strut injector","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"alternating wedge strut injector","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"S ramp injector","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"swept ramp injector","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"counter rotating vortex","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vortex development process","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wall injector","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wall pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"local equivalent ratio","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":"縦渦導入型燃料噴射器の超音速乱流混合・燃焼実験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"縦渦導入型燃料噴射器の超音速乱流混合・燃焼実験"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37095","relation_version_is_last":true,"title":["縦渦導入型燃料噴射器の超音速乱流混合・燃焼実験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:26:08.480835+00:00"}