Conference Paper 高クヌーセン数領域における極超音速希薄流数値解析
Analysis on Hypersonic Rarefied Flows in High Knudsen Number Flow Regime

小澤, 宇志  ,  鈴木, 俊之  ,  藤田, 和央  ,  Ozawa, Takashi  ,  Suzuki, Toshiyuki  ,  Fujita, Kazuhisa

Description
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.
会議情報: 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
形態: カラー図版あり
Meeting Information: 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
Physical characteristics: Original contains color illustrations
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https://repository.exst.jaxa.jp/dspace/bitstream/a-is/561728/1/AA1630005013.pdf

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