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熱化学非平衡を考慮した衝撃波誘起非定常空力加熱の数値計算
https://jaxa.repo.nii.ac.jp/records/37152
https://jaxa.repo.nii.ac.jp/records/37152d1a72cc0-8e3e-4a09-a461-302234d96f23
名前 / ファイル | ライセンス | アクション |
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nalsp0037026.pdf (452.1 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 | 熱化学非平衡を考慮した衝撃波誘起非定常空力加熱の数値計算 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 大気圏突入 | |||||
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 | 衝撃反射パターン | |||||
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 | 非定常流れ場 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱化学非平衡影響 | |||||
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 | 化学種 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 総変分縮小法 | |||||
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 | くさび形 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高マッハ数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱流束 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | atmosphere entry | |||||
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 | shock reflection pattern | |||||
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 | unsteady flowfield | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermochemical nonequilibrium effect | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Navier Stokes equation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | species | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | total variation diminishing scheme | |||||
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 | wedge shape | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high Mach number | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat flux | |||||
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 | Proceedings of the 15th NAL Symposium on numerical simulations of shock wave induced unsteady aerodynamic heating with thermo-chemical nonequilibrium | |||||
著者 |
麻生, 茂
× 麻生, 茂× 海井, 和幸× 藤原, 俊隆× 林, 正徳× Aso, Shigeru× Umii, Kazuyuki× Fujiwara, Toshi× Hayashi, Masanori |
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著者所属 | ||||||
九州大学 工学部 航空工学科 | ||||||
著者所属 | ||||||
九州大学 工学部 航空工学科 | ||||||
著者所属 | ||||||
名古屋大学 工学部 | ||||||
著者所属 | ||||||
西日本工業大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Department of Aeronautics and Astronautics, Faculty of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University Department of Aeronautics and Astronautics, Faculty of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University Faculty of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Nishinippon Institute Technology University | ||||||
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 37, p. 161-164, 発行日 1998-02 |
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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 12-13 Jun. 1997 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 12-13 Jun. 1997 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 衝撃波誘起非定常空力加熱現象を模擬するため、くさびでの非定常衝撃反射過程を数値シミュレーションした。主流マッハ数が大きい場合、流れ場の温度は非常に高温になり、流れ場には熱的・化学的非平衡の効果がもたらされる。本研究では、衝撃反射パターンおよび空力加熱負荷に及ぼす高温効果の影響を調べた。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | An unsteady shock reflection processes at wedge have been numerically simulated in order to simulate shock wave induced unsteady aerodynamic heating phenomena. When freestream Mach number is large, temperature of flowfield becomes very high and thermal and chemical nonequilibrium effects should be induced in the flowfield. The effects of high temperature effects on shock refection patterns and aerodynamic heating loads have been studied in the present study. | |||||
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: AA0001433026 | |||||
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-37 |