JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
titleDNSによる高Mach数・低Reynolds数の球周りの流れ場に対するMach数や温度比の影響把握
Other TitleInvestigation of effect of Mach number and Temperature ratio into Flow Field around a Sphere at High Mach and Low Reynolds Numbers Condition by DNS
Author(jpn)永田, 貴之; 野々村, 拓; 高橋, 俊; 水野, 裕介; 福田, 紘大
Author(eng)Nagata, Takayuki; Nonomura, Taku; Takahashi, Shun; Mizuno, Yusuke; Fukuda, Kota
Author Affiliation(jpn)東海大学; 宇宙航空研究開発機構宇宙科学研究所(JAXA) (ISAS); 東海大学; 東海大学; 東海大学
Author Affiliation(eng)Tokai University; Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) (ISAS); Tokai University; Tokai University; Tokai University
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 page85
End page90
Publication date2016-03-08
Languagejpn
eng
AbstractIn this study, the direct numerical simulations of the flow around a sphere on the high Mach and low Reynolds numbers condition are carried out, and the flow properties are investigated. The three-dimensional compressible Navier-Stokes equations are solved on boundary fitted coordinate system. It is confirmed to have sufficient accuracy by the previous study. Analyses are performed at the Reynolds number (based on the diameter of the sphere and the free-stream velocity) of between 100 and 300, the free-stream Mach number of between 0.3 and 2.0, and the temperature ratio of the sphere surface and free-stream of between 0.5 and 2.0. As a result, we clarified the following points: 1) the effect of the free-stream Reynolds number and temperature ratio on the flow properties, 2) the effect of the temperature ratio can be summarized by the effective Reynolds number that is newly proposed parameter.
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, 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-NOAA1630005012
Report NoJAXA-SP-15-013
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/561733


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