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
抄録（英）
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.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
高クヌーセン数領域における極超音速希薄流数値解析
AA1630005013.pdf
(1.28MB)
