@inproceedings{oai:jaxa.repo.nii.ac.jp:00004009,
 author = {小澤, 宇志 and 鈴木, 俊之 and 藤田, 和央 and Ozawa, Takashi and Suzuki, Toshiyuki and Fujita, Kazuhisa},
 book = {宇宙航空研究開発機構特別資料: 第45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2013論文集, JAXA Special Publication},
 month = {Mar},
 note = {第45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2013 (2013年7月4日-5日. タワーホール船堀), 東京, 45th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2013 (July 4-5, 2013. Tower Hall Funabori), Tokyo, Japan, At Japan Aerospace Exploration Agency (JAXA), a hypersonic rarefied wind tunnel (HRWT) has been developed, and its flow characteristics have been investigated experimentally and numerically. This wind tunnel is capable of producing a 25-mm hypersonic rarefied core flow with a Mach number greater than 10 and a Knudsen number greater than 0.1. However, the temperature of nitrogen gas becomes lower than 50 K in the test section. Hence, in this work we first investigate the effect of N2 condensation in HRWT so as to find out the necessity of a heater activation. Secondly, we discuss development of a measurement system for surface accommodation parameters by measuring the displacement of a pendulous model., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0062268009, レポート番号: JAXA-SP-13-011},
 pages = {47--52},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {極超音速希薄風洞流れ場の粒子計算解析},
 volume = {JAXA-SP-13-011},
 year = {2014}
}