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A computational study of driver gas contamination in a high enthalpy shock tunnel
https://jaxa.repo.nii.ac.jp/records/36751
https://jaxa.repo.nii.ac.jp/records/36751b5754ac6-f054-414b-b6b7-bcb3b4b5a1c9
名前 / ファイル | ライセンス | アクション |
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nalsp0029001.pdf (700.7 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 | ||||||
言語 | en | |||||
タイトル | A computational study of driver gas contamination in a high enthalpy shock tunnel | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高エンタルピー流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値計算 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高温衝撃風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 駆動気体汚染 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 反射衝撃波 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 壁面境界層 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | チョークノズル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞作動条件 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high enthalpy flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational study | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high enthalpy shock wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | driver gas contamination | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reflected shock | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wall boundary layer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | choked nozzle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | tunnel operating condition | |||||
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 | 高温衝撃風洞の駆動気体汚染に関する数値計算 | |||||
著者 |
Chue, R.S.M.
× Chue, R.S.M.× 伊藤, 勝宏× Chue, Randy S. M.× Ito, Katsuhiro |
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著者所属 | ||||||
航空宇宙技術研究所 角田宇宙推進技術研究センター | ||||||
著者所属 | ||||||
航空宇宙技術研究所 角田宇宙推進技術研究センター | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Kakuda Research Center | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Kakuda Research Center | ||||||
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. 3-9, 発行日 1996-01 |
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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 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 | 高エンタルピー反射型衝撃風洞中の駆動気体汚染を調べるために数値計算を行った。この研究は反射衝撃波と壁面境界層および接触面インターフェースの相互作用、および駆動気体汚染に対するそれらの寄与のような非定常事象に焦点を当てた。最適および非最適風洞作動条件やチョークノズルの効果についても論じた。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A computational study has been carried out to examination in a high-enthalpy reflected shock tunnel. The investigation focused on the nonsteady events as the reflected shock interacts with the wall boundary layer and the contact interface and their contribution to driver gas contamination. Both tailored and off-tailored tunnel operating conditions and the effects of a choked nozzle are discussed in the present paper. | |||||
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: AA0000110001 | |||||
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 |