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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
https://jaxa.repo.nii.ac.jp/records/37793
https://jaxa.repo.nii.ac.jp/records/377934f116b52-cddf-449d-bec1-c041e56edf90
名前 / ファイル | ライセンス | アクション |
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nalsp0022032.pdf (465.4 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 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 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速混合流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速流噴射 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 直角方向ジェット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スクラムジェットエンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速燃焼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃料空気混合 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃料濃度分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃焼器内流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 反方向回転渦対 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3次元ピトー圧分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ナビエ・ストークス方程式数値解 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFDコード検証 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD対風洞相関 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算空気力学 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic mixing flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic flow injection | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | crossflow jet | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | scramjet engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic combustion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | fuel air mixing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | fuel concentration distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | combustor flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | counter rotating vortex pair | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three dimensional pitot pressure distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical flow simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Navier Stokes equation numerical solution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD code validation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD wind tunnel correlation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Computational Fluid Dynamics | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | A study on mixing enhancement in supersonic flow fields with secondary transverse injection | |||||
著者 |
山根, 善行
× 山根, 善行× 藤森, 俊郎× 安藤, 安則× 麻生, 茂× 前川, 昌三× 反納, 三智明× 福田, 正大× Yamane, Yoshiyuki× Fujimori, Toshiro× Ando, Yasunori× Aso, Shigeru× Maekawa, Shozo× Tannou, Michiaki× Fukuda, Masahiro |
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著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
石川島播磨重工業 | ||||||
著者所属 | ||||||
九州大学 工学部 航空工学科 | ||||||
著者所属 | ||||||
九州大学 工学部 航空工学科 | ||||||
著者所属 | ||||||
九州大学 工学部 航空工学科 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Ishikawajima-Harima Heavy Industries Co Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Department of Aeronautical Engineering, Faculty of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Department of Aeronautical Engineering, Faculty of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Department of Aeronautical Engineering, Faculty of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
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 en : Special Publication of National Aerospace Laboratory: Proceedings of the 11th NAL Symposium on aircraft computational aerodynamics 巻 22, p. 191-195, 発行日 1994-03 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 航空宇宙技術研究所 10-11 Jun. 1993 東京 日本 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | National Aerospace Laboratory 10-11 Jun. 1993 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 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。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 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. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0004171033 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-22 |