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再突入飛行環境のシミュレーションに用いられる2温度モデルの検証
https://jaxa.repo.nii.ac.jp/records/14690
https://jaxa.repo.nii.ac.jp/records/14690786b718e-d79f-4f28-909f-48e101ee0345
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 再突入飛行環境のシミュレーションに用いられる2温度モデルの検証 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱化学モデル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 2温度モデル | |||||
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 | 極超音速流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機再突入 | |||||
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 | 解離 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力加熱 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 研究開発 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エネルギー緩和 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 電子温度 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermochemical model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | two-temperature model | |||||
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 | hypersonic flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft reentry | |||||
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 | dissociation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic heating | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | research and development | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | energy relaxation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | electron temperature | |||||
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 | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Assessment of the two-temperature model for reentry flow simulations | |||||
著者 |
大津, 広敬
× 大津, 広敬× 宮澤, 政文× Otsu, Hirotaka× Miyazawa, Masafumi |
|||||
著者所属 | ||||||
静岡大学 工学部 | ||||||
著者所属 | ||||||
静岡大学 工学部 | ||||||
著者所属(英) | ||||||
en | ||||||
Shizuoka University Faculty of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Shizuoka University Faculty of Engineering | ||||||
出版者 | ||||||
出版者 | 宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | The Institute of Space and Astronautical Science (ISAS) | |||||
書誌情報 |
宇宙航行の力学シンポジウム 平成14年度 en : Symposium on Flight Mechanics and Astrodynamics 2002 p. 9-12, 発行日 2003-03 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The two-temperature model was assessed for simulating the chemically and thermally nonequilibrium flows around the reentry vehicle. In this analysis, the effect of the parameters for the model on the thickness of the shock layer and the stagnation point heat flux are compared. The flow condition is that the reentry speed is 8.0 km/s at the altitude of 60 km. It was found that the effect of parameters on the thermal nonequilibrium inside the shock layer is significant. But the shock stand-off distance, shock shape, and the heat flux are not affected significantly. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0045913003 |