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SF_6凝縮を伴う超音速ノズル内流れの数値計算 : 第1報, ノズル壁面境界層の影響について
https://sucra.repo.nii.ac.jp/records/12696
https://sucra.repo.nii.ac.jp/records/12696d84ebcae-5d3a-4c80-9dbc-5b1df6100028
名前 / ファイル | ライセンス | アクション |
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A3000137.pdf (511.1 kB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2007-09-10 | |||||
タイトル | ||||||
タイトル | SF_6凝縮を伴う超音速ノズル内流れの数値計算 : 第1報, ノズル壁面境界層の影響について | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Computational Fluid Dynamics | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Supersonic Flow | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Multiphase Flow | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Condensation | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Boundary Layer | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | TVD Scheme | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Classical Condensation Theory | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
タイトル(別言語) | ||||||
その他のタイトル | Numerical Simulation of Compressible Viscous Two-Phase Flow with Condensation : 1st Report, On the Influence of the Boundary Layer | |||||
著者 |
平原, 裕行
× 平原, 裕行× 山下, 桂一× 川橋, 正昭× 呉, 力陽 |
|||||
著者 ローマ字 | ||||||
Hirahara, Hiroyuki | ||||||
著者 ローマ字 | ||||||
Yamashita, Keiichi | ||||||
著者 ローマ字 | ||||||
Kawahashi, Masaaki | ||||||
著者 ローマ字 | ||||||
Wu, Li Yang | ||||||
著者 所属 | ||||||
埼玉大学大学院理工学研究科 | ||||||
著者 所属(別言語) | ||||||
Graduate School of Science and Engineering, Saitama University | ||||||
書誌情報 |
日本機械学會論文集. B編 巻 61, 号 582, p. 399-405, 発行日 1995 |
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年月次 | ||||||
1995-02 | ||||||
出版者名 | ||||||
出版者 | 社団法人日本機械学会 | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 03875016 | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | A compressible viscous two-phase flow of SF_6 and Ar with condensation in a supersonic nozzle is calculated. The flow field is solved with a 3rd-order MUSCL type TVD scheme. The calculation of condensate mass fraction and nucleation rate was based on Becker-Doring's condensation theory. The development of velocity and thermal boundary layer is discussed in detail from the point of view of the interaction between the boundary layer and condensation. Distribution of pressure along the nozzle axis obtained from the numerical calculation is in good accordance with the experimental one in the case of the stagnation pressure region from 20 kPa to 100 kPa. It was found from the result that the condensation takes place in a limited region under relatively high stagnation pressure, which spreads downstream as the stagnation pressure decreases. The temperature and velocity gradients in the boundary layer increase due to the latent heat release of condensation. Consequently, development of the velocity and thermal boundary layers was suppressed by the condensation. | |||||
資源タイプ | ||||||
内容記述タイプ | Other | |||||
内容記述 | text | |||||
フォーマット | ||||||
内容記述タイプ | Other | |||||
内容記述 | application/pdf | |||||
作成日 | ||||||
日付 | 2007-03-05 | |||||
日付タイプ | Created | |||||
アイテムID | ||||||
A3000137 |