JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
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
Other TitleAnalysis on Hypersonic Rarefied Flows in High Knudsen Number Flow Regime
Author(jpn)小澤, 宇志; 鈴木, 俊之; 藤田, 和央
Author(eng)Ozawa, Takashi; Suzuki, Toshiyuki; Fujita, Kazuhisa
Author Affiliation(jpn)宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA)
Author Affiliation(eng)Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA)
Issue Date2016-03-08
Publisher宇宙航空研究開発機構(JAXA)
Japan Aerospace Exploration Agency (JAXA)
Publication title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
VolumeJAXA-SP-15-013
Start page91
End page95
Publication date2016-03-08
Languagejpn
eng
AbstractAt 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.
Description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
Document TypeConference Paper
JAXA Category特別資料
NASA Subject CategoryFluid Mechanics and Thermodynamics
ISSN1349-113X
NCIDAA11984031
SHI-NOAA1630005013
Report NoJAXA-SP-15-013
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/561728


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