Vorticity in Micro Scale Shock Vortex Interaction

被引:1
作者
Wu, Di [1 ]
Shang, Yuhe [1 ]
Xiao, Hong [1 ]
机构
[1] Northwestern Polytech Univ, Sch Power & Energy, Xian 710072, Shanxi, Peoples R China
来源
PROCEEDINGS OF THE 29TH INTERNATIONAL SYMPOSIUM ON RAREFIED GAS DYNAMICS | 2014年 / 1628卷
关键词
shock/vortex interaction DSMC; DIRECT NUMERICAL-SIMULATION; SOUND GENERATION;
D O I
10.1063/1.4902600
中图分类号
O59 [应用物理学];
学科分类号
摘要
Extensively investigations of the net voracity in micro-scale shock/vortex interaction were conducted by validated direct simulation of Monte Carlo (DSMC). The major characteristic is found that the strong shock/vortex interaction in micro-scale can cause an increase in enstrophy, which differs from the previous DSMC studies. investigations also show that the increase of the enstrophy causes an increase dissipation rate in during the strong interaction. The shock Mach number, vortex size and vortex Mach number turn out to play a critical role in the strength of interaction, which in turn govern the change in the dissipation rate. The ratio, of shock thickness to vortex core radius, is founded to be an important parameter which determines the tendency of enstrophy. When the ratio is more than about 0.5, the increasing of enstrophy disappear, which is different from the previous studies of macro-scale shock/vortex interaction. When the shock wave is strong enough to make the ratio less than 0.5, the macro interaction phenomenon tends to reproduce.
引用
收藏
页码:249 / 254
页数:6
相关论文
共 15 条
[1]  
Bird G., 1994, MOL GAS DYNAMICS DIR
[2]   The shock-vortex interaction patterns affected by vortex flow regime and vortex models [J].
Chang, Keun-Shik ;
Barik, Hrushikesh ;
Chang, Se-Myong .
SHOCK WAVES, 2009, 19 (04) :349-360
[3]   Multiple Sound Generation in Interaction of Shock Wave with Strong Vortex [J].
Chatterjee, A. ;
Vijayaraj, S. .
AIAA JOURNAL, 2008, 46 (10) :2558-2567
[4]   Rarefaction and compressibility effects on steady and transient gas flows in microchannels [J].
Colin, S .
MICROFLUIDICS AND NANOFLUIDICS, 2005, 1 (03) :268-279
[5]   Study of subsonic-supersonic gas flow through micro/nanoscale nozzles using unstructured DSMC solver [J].
Darbandi, Masoud ;
Roohi, Ehsan .
MICROFLUIDICS AND NANOFLUIDICS, 2011, 10 (02) :321-335
[6]   THE INTERACTION OF A SHOCK WITH A VORTEX - SHOCK DISTORTION AND THE PRODUCTION OF ACOUSTIC-WAVES [J].
ELLZEY, JL ;
HENNEKE, MR ;
PICONE, JM ;
ORAN, ES .
PHYSICS OF FLUIDS, 1995, 7 (01) :172-184
[7]   Sound generation by shock-vortex interactions [J].
Inoue, O ;
Hattori, Y .
JOURNAL OF FLUID MECHANICS, 1999, 380 :81-116
[8]   The vorticity jump across a shock in a non-uniform flow [J].
Kevlahan, NKR .
JOURNAL OF FLUID MECHANICS, 1997, 341 :371-384
[9]  
Koffi K., 2005, 35 AIAA FLUID DYN C
[10]   Dynamics of microscale shock/vortex interaction [J].
Koffi, Kossi ;
Andreopoulos, Yiannis ;
Watkins, Charles B. .
PHYSICS OF FLUIDS, 2008, 20 (12)