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HSCT模型の数値解析 その1
https://jaxa.repo.nii.ac.jp/records/37344
https://jaxa.repo.nii.ac.jp/records/37344333bb629-d1e4-4429-b2d1-2dace4b23e5b
名前 / ファイル | ライセンス | アクション |
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nalsp0041030.pdf (611.0 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | HSCT模型の数値解析 その1 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HSCT | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高速民間輸送機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ナビエ・ストークス解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | MUSCL | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流束差分離法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | LU-ADI陰解法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧力分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 負圧ピーク | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 単純風上保存則スキーム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 上下交互方向陰的差分法 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HSCT | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high speed civil transport | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Navier Stokes analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | MUSCL | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flux difference splitting | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | LU ADI method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pressure distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | suction peak | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | monotone upwind scheme for conservation law | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | lower upper alternating direction implicit method | |||||
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 | Numerical simulation of HSCT wind tunnel test model, phase 1 | |||||
著者 |
海田, 武司
× 海田, 武司× 渡邉, 直樹× Kaiden, Takeshi× Watanabe, Naoki |
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著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
三菱重工業 | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries Ltd | ||||||
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 巻 41, p. 203-208, 発行日 1999-02 |
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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 | 航空宇宙技術研究所 24-26 Jun. 1998 東京 日本 | |||||
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 | National Aerospace Laboratory 24-26 Jun. 1998 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | HSCT(高速民間輸送機)空力設計用のCFD(数値流体力学)ツールを実証するために、HSCT-F1/P1標準模型のナビエ・ストークス解析を実行した。格子システムの位相は単一構造化したC-Oタイプの構造格子である。MUSCL(Monotone Upwind Schemes for Conservation Laws)法を備えたRoeの流束差分離法を空間を離散的にするために使用した。時間積分には、LU-ADI(Lower-Upper Alternating Direction Implicit)陰解法を採用した。乱流モデルはBaldwin-Lomaxの代数的モデルである。数値結果を風洞試験の結果と比較した。力データおよび圧力分布は両方ともよい一致を示したが、上面前縁において負圧ピークの不一致が見つかった。これを研究するために、工作許容精度を含むモデルや異なる迎角の場合に関して解析を行った。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Navier-Stokes analysis of HSCT (High Speed Civil Transport) F1, P1 standard model was carried out in order to validate CFD (Computational Fluid Dynamics) tool for HSCT aerodynamics design. The topology of grid system is the single structured C-O type. Roe's flux difference splitting with MUSCL (Monotone Upwind Schemes for Conservation Laws) is used to enable discrete representation of the space. LU-ADI (Lower-Upper Alternating Direction Implicit) method is adopted in time integration. The turbulence model is the algebraic model of Baldwin-Lomax. The numerical results are compared with those of wind tunnel test. Though both of forces and pressure distribution give the good agreement, the discrepancy of suction peak at upper leading edge is found. In order to investigate this, the model including the fabrication tolerance and the case with another angle of attack are analyzed. | |||||
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: AA0001958030 | |||||
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-41 |