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計算格子に斜交する衝撃波の鋸歯状化現象の解析
https://jaxa.repo.nii.ac.jp/records/3642
https://jaxa.repo.nii.ac.jp/records/36428153e3d2-ab43-4bdd-8309-cf82da8cebe5
名前 / ファイル | ライセンス | アクション |
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AA1630005017.pdf (508.0 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2016-04-21 | |||||
タイトル | ||||||
タイトル | 計算格子に斜交する衝撃波の鋸歯状化現象の解析 | |||||
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_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 | Analysis on effect of grid to the capturing of shock surfaces that are oblique to the axes of Cartesian grid for computation | |||||
著者 |
相曽, 秀昭
× 相曽, 秀昭× Aiso, Hideaki |
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著者所属 | ||||||
宇宙航空研究開発機構航空技術部門数値解析技術研究ユニット(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Simulation Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 47th Fluid Dynamics Conference / the 33rd Aerospace Numerical Simulation Symposium 巻 JAXA-SP-15-013, p. 115-120, 発行日 2016-03-08 |
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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 | 第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム (2015年7月2日-3日. 東京大学生産技術研究所), 目黒区, 東京 | |||||
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 | 47th Fluid Dynamics Conference /the 33rd Aerospace Numerical Simulation Symposium (July 2-3, 2015. Institute of Industrial Science , the University of Tokyo), Meguro-ku, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | We are concerned with numerical computation of shocks whose surfaces are oblique to any axis of grid for computation, where the grid is a structured orthognal grid. It is easily observed that the capturing of shock surface is affected by the grid and that the surface often looks jagged but not smooth, even if the shock surface should be planar or smooth from theory. The phenomenon is purely numerical and the machinery of phenomenon is not yet clear. While the setting of problem is rather simple, several different mathematical factors are complicatedly related even in the case of compressible Euler equations for ideal gases. Therefore we analysis we still obtain some essential part of the numerical machinery, which may suggest a method to decrease the inconvenient effect of grid. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1630005017 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-15-013 |