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化学反応を含む圧縮流の数値計算
https://jaxa.repo.nii.ac.jp/records/43296
https://jaxa.repo.nii.ac.jp/records/43296f700f489-f537-4a30-8036-00ea91b350f8
名前 / ファイル | ライセンス | アクション |
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nalsp0009005.pdf (674.0 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 化学反応を含む圧縮流の数値計算 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Numerical Calculation of Chemically Reacting Compressible Flow | |||||
著者 |
石黒, 登美子
× 石黒, 登美子× 小川, 哲× 和田, 安弘× Ishiguro, Tomiko× Ogawa, Satoru× Wada, Yasuhiro |
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著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
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 en : Special Publication of National Aerospace Laboratory SP-9 巻 9, p. 27-36, 発行日 1988-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A summary of our solver-code which is being developed for the purpose of analyzing chemically reacting compressible flows numerically is presented. The code solves the two or three-dimensional Reynolds time average complete Navier-Stokes equations including species transport equations, and has two strong points. The first point is that the system of governing equations for the flow computation contains a total mass conservation equation and transport equations of all species taking account of total mass conservation and impartial numerical treatment of every chemical species. Therefore, the correction of mass ratios of an species is made so that the summation of them equals to 1 after every time step integration. The second point is that the TVD difference scheme is used in order to capture strong discontinuous surfaces clearly and efficiently which are apt to appear in supersonic flow fields. Applying this solver, shock-induced chemically reacting flows and flow fields for the case of transverse sonic injection of H2 fuel into a supersonic airstream are analyzed numerically. | |||||
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: NALSP0009005 | |||||
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-9 |