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二酸化炭素極超音速希薄流における凝縮モデルの検討
https://jaxa.repo.nii.ac.jp/records/38783
https://jaxa.repo.nii.ac.jp/records/38783ed2f3e8b-1dc2-4148-997b-df44fb36bbdc
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2016-08-15 | |||||
タイトル | ||||||
タイトル | 二酸化炭素極超音速希薄流における凝縮モデルの検討 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Rarefied gas dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Hypersonic flows | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Aerodynamics | |||||
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 | Modeling of Condensation in CO2 Hypersonic Rarefied Flows | |||||
著者 |
小澤, 宇志
× 小澤, 宇志× 鈴木, 俊之× 藤田, 和央× Ozawa, Takashi× Suzuki, Toshiyuki× Fujita, Kazuhisa |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会(JSASS) | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Aeronautical and Space Sciences (JSASS) | |||||
書誌情報 |
第59回宇宙科学技術連合講演会講演集 en : Proceedings of 59th Space Sciences and Technology Conference 発行日 2015-10-07 |
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関係URI | ||||||
識別子タイプ | URI | |||||
関連識別子 | https://www.jsass.jp/conference/sstc59.php | |||||
関連名称 | https://www.jsass.jp/conference/sstc59.php | |||||
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 | 第59回宇宙科学技術連合講演会(2015年10月7日-9日. かごしま県民交流センター), 鹿児島市, 鹿児島県 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | At Japan Aerospace Exploration Agency (JAXA), a hypersonic rarefied wind tunnel (HRWT) has been developed for the prediction of rarefied aerodynamics. Lately, we plan to extend the capability of HRWT to CO2 hypersonic flows so as to improve CO2 aerodynamic prediction for Mars missions. For CO2 rarefied aerodynamics, condensation effect may not be negligible, and thus, the understanding of CO2 condensing flows is essential. In this study, we first develop numerical schemes for CO2 condensing flows. Second, we investigate the impact of condensation on rarefied aerodynamics in the HRWT test section. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11800503 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1600041000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JSASS-2015-4630 |