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ブロック境界条件を応用したマルチブロックLES解析コードの開発と検証
https://jaxa.repo.nii.ac.jp/records/3480
https://jaxa.repo.nii.ac.jp/records/3480c7583e14-d0f7-49c2-8520-dbb5bdb3ea11
名前 / ファイル | ライセンス | アクション |
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AA1630031005.pdf (2.3 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2017-01-13 | |||||
タイトル | ||||||
タイトル | ブロック境界条件を応用したマルチブロックLES解析コードの開発と検証 | |||||
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 | The development of the large-eddy simulation analysis solver based on the block interface condition and its verification | |||||
著者 |
青野, 光
× 青野, 光× 野々村, 拓× Aono, Hikaru× Nonomura, Taku |
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著者所属 | ||||||
東京理科大学 | ||||||
著者所属 | ||||||
東北大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo University of Science | ||||||
著者所属(英) | ||||||
en | ||||||
Tohoku University | ||||||
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48回流体力学講演会/第34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 48th Fluid Dynamics Conference / the 34th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-16-007, p. 63-67, 発行日 2016-12-27 |
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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48回流体力学講演会/第34回航空宇宙数値シミュレーション技術シンポジウム (2016年7月6日-8日. 金沢歌劇座), 金沢市, 石川 | |||||
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 | 48th Fluid Dynamics Conference /the 34th Aerospace Numerical Simulation Symposium (July 6-8, 2016. The Kanazawa Theatre), Kanazawa, Ishikawa, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A large-eddy simulation analysis solver using the multi-block grid with several block interface conditions is developed. The governing equations are the three-dimensional compressible Navier-Stokes equations in the generalized curvilinear coordinates. We adopt a sixth-order compact finite difference scheme for the convective and viscous terms and a fourth-order Runge-Kutta method for time integration. We introduce a block interface condition (BIC) that is newly developed and constructed based on the analogy between the finite volume scheme and the finite difference scheme. The BIC is compared with a characteristic based interface condition (CIC). We consider a single vortex convection crossing the boundary interface between the uniform Cartesian grid and the uniform Cartesian grid with considerable tilt as a test problem. Effects of strength of the vortex on the pressure distribution of the moving vortex are studied. A comparison of the pressure distribution of the vortex at the boundary interface presents that in the case of strong vortex the results of BIC are comparable to those of the CIC while in the case of weak vortex numerical oscillations are observed when the vortex crosses the interface. Furthermore, results obtained using the CIC and the BIC are considerably improved with increasing grid resolution in normal to the block interface. | |||||
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: AA1630031005 | |||||
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-16-007 |