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δ2-Correction Scheme for Unsteady Compressible Navier-Stokes Equations
https://jaxa.repo.nii.ac.jp/records/45265
https://jaxa.repo.nii.ac.jp/records/45265758da786-7a12-4dd4-9e15-5655c6647b97
名前 / ファイル | ライセンス | アクション |
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naltr01006.pdf (823.8 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 | ||||||
言語 | en | |||||
タイトル | δ2-Correction Scheme for Unsteady Compressible Navier-Stokes Equations | |||||
言語 | ||||||
言語 | eng | |||||
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 | ||||||
その他のタイトル | 非定常ナビエ・ストークス方程式に対するδ2-コレクションスキーム | |||||
著者 |
松野, 謙一
× 松野, 謙一× MATSUNO, Kenichi |
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著者所属 | ||||||
航空宇宙技術研究所空力性能部 | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
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報告 en : Technical Report of National Aerospace Laboratory TR-1006 巻 1006, p. 13, 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 an algorithm of the ”δ2-form”, of which the right hand side is a numerical approximation of unsteady governing equations. This algorithm makes a scheme especially suitable for time accurate simulations. A shock tube flow is calculated as an example. The flow is assumed laminar, and a shock wave-boundary layer interaction is simulated. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR1006000 | |||||
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 TR-1006 |