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OREXまわりの極超音速ナビエ・ストークス解析
https://jaxa.repo.nii.ac.jp/records/37829
https://jaxa.repo.nii.ac.jp/records/3782908080fed-8944-4732-b2e3-ac8774404bd6
名前 / ファイル | ライセンス | アクション |
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nalsp0026005.pdf (425.6 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 | OREXまわりの極超音速ナビエ・ストークス解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 再突入空気力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非平衡流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 実在気体効果 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ナビエ・ストークス方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | OREX | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道再突入実験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流速ベクトル分割 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 人工粘性項制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値不安定 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 粘性衝撃層解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非平衡粘性衝撃層 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reentry aerodynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nonequilibrium flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | real gas effect | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical flow simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD analysis | |||||
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 | Navier Stokes equations | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | OREX | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbital reentry experiment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flux vector splitting | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | artificial viscosity control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical instability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | viscous shock layer analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nonequilibrium viscous shock layer | |||||
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 | Hypersonic Navier-Stokes simulations around OREX | |||||
著者 |
瀬川, 清
× 瀬川, 清× 中野, 晋× 坪内, 邦良× Segawa, Kiyoshi× Nakano, Susumu× Tsubouchi, Kuniyoshi |
|||||
著者所属 | ||||||
日立製作所 機械研究所 | ||||||
著者所属 | ||||||
日立製作所 機械研究所 | ||||||
著者所属 | ||||||
日立製作所 機械研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Hitachi Ltd Mechanical Engineering Research Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
Hitachi Ltd Mechanical Engineering Research Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
Hitachi Ltd Mechanical Engineering Research 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 巻 26, p. 35-39, 発行日 1994-12 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 軸対称ナビエ・ストークス方程式を解くことにより、マッハ数7.1の空気の流れの中におけるOREXのまわりの流れの数値シミュレーションを行った。強い衝撃波と膨張波が生成され相互に干渉し合う領域で誤差が集積することのないよう数値解法にはvan Leerの流束分割法を修正したHaenelの分割法を採用した。また高精度解法として有限容積法に対しTVD-MUSCL法を適用した。時間積分には2段階のルンゲ・クッタ法を用いた。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Numerical simulations of the flows around Orbital Reentry Experiment (OREX) has been performed in a Mach 7.1 air stream by solving axisymmetric Navier-Stokes equations. Haenel's Flux Vector Splitting, which is a modified form of the original van Leer's splitting, is adopted to the numerical method in order to avoid an accumulated error appearing in the regions where strong shock and expansion waves are generated and interact with each other. Additionally, the TVD-MUSCL (Total Variation Diminishing-Monotone Upstream-centered Scheme for Conservation Laws) approach is applied to the finite volume method as a high resolution scheme. The two-step Runge-Kutta method is used for time integration. | |||||
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: AA0004173005 | |||||
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-26 |