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非定常圧縮性ナビエ・ストークス方程式に対する高精度陰解法
https://jaxa.repo.nii.ac.jp/records/43305
https://jaxa.repo.nii.ac.jp/records/433056c7c5cfe-2c04-418a-8a08-cdad0fd21dad
名前 / ファイル | ライセンス | アクション |
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nalsp0009014.pdf (380.2 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 | 非定常圧縮性ナビエ・ストークス方程式に対する高精度陰解法 | |||||
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 | An Implicit Scheme for Unsteady Compressible Navier-Stokes Equations | |||||
著者 |
松野, 謙一
× 松野, 謙一× Matsuno, Ken-ichi |
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著者所属 | ||||||
航空宇宙技術研究所数理解析部 | ||||||
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. 93-96, 発行日 1988-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper a time accurate scheme for unsteady Navier-Stokes equations is presented. This scheme employs, as unknowns, quantities of order of square of time spacing, thus making a "delta2-form", of which the right hand side is a numerical approximation of unsteady governing equations. This argorithm makes a scheme especially suitable for time accurate simulations A shock tube flow is calculated as an example. The flow is assumed laminar, and shock wave-boundary layer interaction is simulated. | |||||
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: NALSP0009014 | |||||
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 |