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二酸化炭素気流中衝撃波背後の発光スペクトル解析
https://jaxa.repo.nii.ac.jp/records/14332
https://jaxa.repo.nii.ac.jp/records/143323171a4d1-f085-49a7-aea1-491c71655e60
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 | 二酸化炭素気流中衝撃波背後の発光スペクトル解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Emission spectroscopy | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Shock tube | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Carbon dioxide | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Nonequilibrium | |||||
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 | Analysis of emission spectra behind a shock wave in carbon dioxide gas flow | |||||
著者 |
高栁, 大樹
× 高栁, 大樹× 藤田, 和央× Takayanagi, Hiroki× Fujita, Kazuhisa |
|||||
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) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航行の力学シンポジウム: 平成22年度 en : Symposium on Flight Mechanics and Astrodynamics: 2010 発行日 2011-08 |
|||||
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 | 宇宙航行の力学シンポジウム 平成22年度 (2010年12月16-17日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県 | |||||
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 | Symposium on Flight Mechanics and Astrodynamics, 2010 (December 16-17, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The shock tube experiments are carried out to study the radiation behind a strong shock wave in a pure carbon dioxide. C2 swan emission intensity measurements around 500nm and CO(4+) emission in VUV region are measured behind a strong shock wave around 6.5km/s in a CO2 flow. The emission spectra are analyzed and compared with the simulated spectra by SPARADIAN2. By comparison in VIS region, the temperature is estimated as 13,500K, while in UV region, it is estimated as 6,000-8,000K. The major cause of difference could be background continuum radiation observed in VIS region, which may originate from larger electron densities. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0065106013 |