@inproceedings{oai:jaxa.repo.nii.ac.jp:00005411,
 author = {藤田, 和央 and 水野, 雅仁 and 石田, 清道 and 藤井, 啓介 and 長井, 遵正 and Fujita, Kazuhisa and Mizuno, Masahito and Ishida, Kiyomichi and Fujii, Keisuke and Nagai, Jyunsei},
 book = {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, JAXA Special Publication: Proceedings fo 40th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2008},
 month = {Feb},
 note = {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, 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., 形態: カラー図版あり, 資料番号: AA0064303009, レポート番号: JAXA-SP-08-009},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {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},
 volume = {JAXA-SP-08-009},
 year = {2009}
}