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High enthalpy flow workshop problem. 2-1: OREX configuration
https://jaxa.repo.nii.ac.jp/records/36758
https://jaxa.repo.nii.ac.jp/records/367582292a35e-fe9a-4237-bd5c-baaae9eda6d5
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp0029008.pdf (453.7 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | High enthalpy flow workshop problem. 2-1: OREX configuration | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | MUSCL | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 保存則のための単調な上流スキーム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 補外法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風上法 | |||||
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 | 非平衡化学反応 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | FVS | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流束ベクトル分割法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | AUSM | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 移流上流分割法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 理想気体流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 衝撃波 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 膨張波 | |||||
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 | monotonic upstream schemes for conservation law | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | extrapolation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | upwind method | |||||
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 | nonequilibrium chemical reacting | |||||
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 | FVS | |||||
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 | AUSM | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | advection upstream splitting method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ideal gas flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shock wave | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | expansion wave | |||||
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 | ||||||
その他のタイトル | 高エンタルピー流ワークショップの課題 2-1:OREXコンフィギュレーション | |||||
著者 |
中森, 一郎
× 中森, 一郎× 中村, 佳朗× Nakamori, Ichiro× Nakamura, Yoshiaki |
|||||
著者所属 | ||||||
名古屋大学 工学研究科 | ||||||
著者所属 | ||||||
名古屋大学 工学研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University Graduate School of Engineering | ||||||
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 29, p. 108-113, 発行日 1996-01 |
|||||
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 8 Jun. 1995 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 8 Jun. 1995 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | MUSCL(保存則のための単調な上流スキーム)型補外法を持つ風上法を軌道再突入実験(OREX)コンフィギュレーション回りの非平衡化学反応極超音速流に適用した。この計算に使った流れ解法は、Steger-Warmingの流束ベクトル分割法(FVS)を基にし、移流上流分割法(AUSM)の変形として分類される。現在のスキームは、衝撃波に対する単調性、膨張波に対するロバスト性および接触不連続や剪断層に対する高分解能のような理想気体流において多くの良い特徴を持っている。現在のスキームを化学反応流れに拡張するために、17の化学反応をもつ5つの中性種(N,O,NO,O2,N2)に対しParkの2温度モデルを使い、軸対象ナビエ・ストークス方程式と区別するために有限体積定式化を使った。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this computation, an upwind method with MUSCL (Monotonic Upstream Schemes for Conservation Laws) type extrapolation was applied to nonequilibrium chemical reacting hypersonic flow around an Orbital Reentry Experiment (OREX) configuration. The flow solver employed in this computation is based on Steger and Warming's flux-vector splitting (FVS), and classified as a variation of the Advection Upstream Splitting Method (AUSM). It has been confirmed that the present scheme has many good characteristics in the ideal gas flow such as monotonicity for shock wave, robustness for expansion wave, and high resolution for contact discontinuity and shear layer. In order to extend the present scheme to a chemical reacting flow, Park's two temperature model for five neutral species (N, O, NO, O2, N2) were used with 17 chemical reaction, and the finite volume formulation was employed to discretize the axisymmetric Navier-Stokes equations. | |||||
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: AA0000110008 | |||||
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-29 |