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熱防御システムの高信頼性評価に向けた誘導加熱風洞の高精度気流検定
https://jaxa.repo.nii.ac.jp/records/5411
https://jaxa.repo.nii.ac.jp/records/541165400bc6-e196-4110-8f40-ce6852950ce2
名前 / ファイル | ライセンス | アクション |
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64303009.pdf (1.2 MB)
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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 | 熱防御システムの高信頼性評価に向けた誘導加熱風洞の高精度気流検定 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Spectrum fitting, Emission spectroscopy, High-enthalpy Flows, Flow diagnostics | |||||
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 | Accurate flow characterization of ICP wind tunnel for high-integrity TPS performance evaluation | |||||
著者 |
藤田, 和央
× 藤田, 和央× 水野, 雅仁× 石田, 清道× 藤井, 啓介× 長井, 遵正× Fujita, Kazuhisa× Mizuno, Masahito× Ishida, Kiyomichi× Fujii, Keisuke× Nagai, Jyunsei |
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著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
エイ・イー・エス | ||||||
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) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Advanced Engineering Services | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第40回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2008論文集 en : JAXA Special Publication: Proceedings fo 40th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2008 巻 JAXA-SP-08-009, 発行日 2009-02-27 |
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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 | 第40回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2008. 会期: 2008年6月12日-6月13日. 会場: 東北大学片平キャンパス | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In order to offer the detailed information about test flows in a 110-kW inductively-coupled-plasma heater at Aerospace Research Center of Japan Aerospace Exploration Agency, radiation spectroscopy associated with the line-by-line spectrum analysis was conducted. Radial distributions of the temperature and the species concentration were obtained in the test section by the numerical spectrum fitting procedure in a wide range of the input electric power with air and nitrogen as the working gas. Contributions of emission from impurities were incorporated into numerical spectra, from which radial distribution of impurities was determined as well. In an attempt to eliminate such impurities from the nitrogen test flow, ambient gas in the test chamber was replaced with the nitrogen gas before ignition of the heater. As a result, considerable reduction of NO and O was accomplished. | |||||
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 | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064303009 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-08-009 |