高クヌーセン数領域における極超音速希薄流数値解析

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  • Analysis on Hypersonic Rarefied Flows in High Knudsen Number Flow Regime

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Abstract

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

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