{"created":"2023-06-20T15:08:21.882784+00:00","id":37793,"links":{},"metadata":{"_buckets":{"deposit":"a45d39e6-4d68-4fae-b37a-d1ee4a1bf602"},"_deposit":{"created_by":1,"id":"37793","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37793"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037793","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["483017","483021","483026","483019","483025","483016","483020","483023","483028","483024","483015","483022","483018","483027"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A study on mixing enhancement in supersonic flow fields with secondary transverse injection"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"195","bibliographicPageStart":"191","bibliographicVolumeNumber":"22","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 第11回航空機計算空気力学シンポジウム論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of the 11th NAL Symposium on aircraft computational aerodynamics","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 10-11 Jun. 1993 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 10-11 Jun. 1993 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"直角方向の噴射がある超音速混合流れ場の基本的特性を数値的および実験的に調べた。平板上の単一孔から超音速流れ(M=4)に直角に音速ジェットを吹き出す。ピトー圧分布を3次元的に測定した。流れ場の数値シミュレーションを行い実験データと比較した。本研究が定量的に裏付けられ、良好な信頼性をもつことがわかった。数値的および実験的な結果に基づいて本研究における流れ場の現象を論じた。互に反対向きの回転をもつ渦対が平板の近傍で生成され、この渦による巻き込みの結果として混合が生ずる。ジェットの中心はピトー圧の分布から推定した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A fundamental characteristic of supersonic mixing field with transverse injection is examined by numerical and experimental studies. A sonic jet is injected perpendicularly into supersonic flow (Mach number = four) from a single hole on flat plate. The pitot pressure distribution is measured three dimensionally. Numerical simulation is conducted in the flow field, and is compared with experimental data. It is shown that the present investigation is verified quantitatively and has a good reliability. On the basis of numerical and experimental results, phenomena of the present flow field are discussed. It is observed that the counter rotating vortex pair which rolls up from near the flat plate is generated and the mixing occurs as a result of entraining by these vortexes. Jet core location is estimated from pitot pressure distribution.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004171033","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-22","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":"石川島播磨重工業"},{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"石川島播磨重工業"},{"subitem_text_value":"九州大学 工学部　航空工学科"},{"subitem_text_value":"九州大学 工学部　航空工学科"},{"subitem_text_value":"九州大学 工学部　航空工学科"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Ishikawajima-Harima Heavy Industries Co Ltd"},{"subitem_text_language":"en","subitem_text_value":"Kyushu University Department of Aeronautical Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Kyushu University Department of Aeronautical Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Kyushu University Department of Aeronautical Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山根, 善行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤森, 俊郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安藤, 安則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"麻生, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"前川, 昌三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"反納, 三智明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"福田, 正大"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamane, Yoshiyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fujimori, Toshiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ando, Yasunori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aso, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Maekawa, Shozo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tannou, Michiaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Fukuda, Masahiro","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":"nalsp0022032.pdf","filesize":[{"value":"465.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0022032.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37793/files/nalsp0022032.pdf"},"version_id":"6ede6350-7977-400c-90d9-e67a8f366e97"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速混合流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速流噴射","subitem_subject_scheme":"Other"},{"subitem_subject":"直角方向ジェット","subitem_subject_scheme":"Other"},{"subitem_subject":"スクラムジェットエンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速燃焼","subitem_subject_scheme":"Other"},{"subitem_subject":"燃料空気混合","subitem_subject_scheme":"Other"},{"subitem_subject":"燃料濃度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"燃焼器内流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"反方向回転渦対","subitem_subject_scheme":"Other"},{"subitem_subject":"3次元ピトー圧分布","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス方程式数値解","subitem_subject_scheme":"Other"},{"subitem_subject":"CFDコード検証","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD対風洞相関","subitem_subject_scheme":"Other"},{"subitem_subject":"計算空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic mixing flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flow injection","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"crossflow jet","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"scramjet engine","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic combustion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fuel air mixing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"fuel concentration distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"combustor flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"counter rotating vortex pair","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three dimensional pitot pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation numerical solution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD code validation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD wind tunnel correlation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Computational Fluid Dynamics","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":"超音速流中に垂直に2次流を噴射したときの混合流れ場の構造に関する基礎研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速流中に垂直に2次流を噴射したときの混合流れ場の構造に関する基礎研究"}]},"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":"37793","relation_version_is_last":true,"title":["超音速流中に垂直に2次流を噴射したときの混合流れ場の構造に関する基礎研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:12:14.078515+00:00"}