@inproceedings{oai:jaxa.repo.nii.ac.jp:00003859,
 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46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム論文集, JAXA Special Publication: Proceedings of the 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium},
 month = {Mar},
 note = {第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム (2014年7月3日-4日. 弘前文化センター), 弘前市, 青森県, 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium (July 3-4, 2014. Hirosaki Bunka Center), Hirosaki, Aomori, Japan, At Japan Aerospace Exploration Agency (JAXA), a hypersonic rarefied wind tunnel (HRWT) has been developed for the purpose of studying rarefied gas dynamics. In accordance with our previous work, this wind tunnel is capable of producing 25-mm hypersonic rarefied core flows with a Mach number greater than 10 and a Knudsen number greater than 0.1 with a 5-mm model. In this work, we first investigate a measurement system for surface accommodation parameters by measuring the displacement of sphere pendulous models, and discuss the capability to determine surface parameters of various materials., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1530023024, レポート番号: JAXA-SP-14-010},
 pages = {133--137},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {極超音速希薄空力特性に及ぼす表面モデルの影響},
 volume = {JAXA-SP-14-010},
 year = {2015}
}