@inproceedings{oai:jaxa.repo.nii.ac.jp:00003638,
 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47回流体力学講演会/第33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 47th Fluid Dynamics Conference / the 33rd Aerospace Numerical Simulation Symposium},
 month = {Mar},
 note = {第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム (2015年7月2日-3日. 東京大学生産技術研究所), 目黒区, 東京, 47th Fluid Dynamics Conference /the 33rd Aerospace Numerical Simulation Symposium (July 2-3, 2015. Institute of Industrial Science , the University of Tokyo), Meguro-ku, Tokyo, Japan, At Japan Aerospace Exploration Agency (JAXA), a hypersonic rarefied wind tunnel (HRWT) has been developed for the purpose of improving understanding of rarefied gas flow characteristics. In this work, we first develop a rarefaction model for pitot pressure measurements for hypersonic rarefied flows. Second, we investigate a measurement method using Patterson-type probes in high Knudsen number flow regime for HRWT., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630005013, レポート番号: JAXA-SP-15-013},
 pages = {91--95},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {高クヌーセン数領域における極超音速希薄流数値解析},
 volume = {JAXA-SP-15-013},
 year = {2016}
}