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設計における数値解析の活用について(その5): 陰的TVD法の改良と応用計算
https://jaxa.repo.nii.ac.jp/records/43276
https://jaxa.repo.nii.ac.jp/records/43276cfe190f2-5d8f-48c7-8ae2-0253bec27b75
名前 / ファイル | ライセンス | アクション |
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nalsp0008023.pdf (554.9 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 | 設計における数値解析の活用について(その5): 陰的TVD法の改良と応用計算 | |||||
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 | The Role of Computational Fluid Dynamics in Aeronautical Engineering (5) - Improvements and Applications of Implicit TVD Finite Volume Code - | |||||
著者 |
嶋, 英志
× 嶋, 英志× 吉田, 憲司× 天野, 完一× Shima, Eiji× Yoshida, Kenji× Amano, Kan-ichi |
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著者所属 | ||||||
川崎重工業株式会社 | ||||||
著者所属 | ||||||
川崎重工業株式会社 | ||||||
著者所属 | ||||||
日本航空機開発協会 | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd., Kakamigahara | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd., Kakamigahara | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aircraft Development Corporation | ||||||
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-8 巻 8, p. 169-176, 発行日 1987-11 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An automatic grid generator for multiple element airfoils was developed and the existing implicit TVD (Total Variation Diminishing) finite volume code was improved in both accuracy and efficiency, in order to make the Navier-Stokes solver a practical design tool for high lift devices. Utilizing these codes, Navier-Stokes analysis of the single slotted flap was carried out. The automatic grid generator utilizes the elliptic equation solver using the finite difference method combined with the panel method. The flow field is divided into subregions by the dividing stream lines which is calculated by the panel method and the computational grid in each subregion is generated by solving the elliptic equations (Thompson's method). Since the panel method can solve the potential flow around any number of arbitrary shaped bodies, this grid generator can generate a H-type computational grid around such bodies automatically. To obtain a high accuracy on a rapidly stretching grid, the flow solver uses the TVD formulation containing a explicit treatment of non-uniform grid spacing. Converging rate and numerical stability of the flow solver is augmented by the relaxation approach using Symmetric Point Gauss Seidel method in matrix inversion process which is necessary for an implicit scheme. | |||||
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: NALSP0008023 | |||||
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-8 |