Numerical investigations on dynamics and heat transfer in a turbulent underexpanded jet

被引:24
作者
Bartosiewicz, Y [1 ]
Mercadier, Y
Proulx, P
机构
[1] Univ Sherbrooke, Fac Engn, Dept Mech Engn, Sherbrooke, PQ J1K 2R1, Canada
[2] Univ Sherbrooke, Fac Engn, Dept Chem Engn, Sherbrooke, PQ J1K 2R1, Canada
关键词
D O I
10.2514/2.1562
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A fully elliptic Navier-Stokes equation solver in conjunction with a Reynolds stress model is validated for mildly and strongly underexpanded jets. For mildly underexpanded jets, good agreement has been found compared to available measurements for the shock reflections. The model even demonstrated some improvements over a three-dimensional modified k-epsilon model for turbulent predictions, which confirms the inadequacy of isotropic eddy-viscosity-based models to represent properly the turbulence in those flows. For the strongly underexpanded case, the predicted Mach disk location and size are found to be in excellent agreement compared to available measurements. In addition, the predicted flow structure beyond the disk agrees with experimental observations. An attempt is also made to explain the strong coupling between some dynamic features and heat transfer aspects. The sonic line location is revealed to be an important parameter in understanding the global dynamics/heat transfer coupling. In addition, it is demonstrated that a fraction of heat dissipation may be given back to the How and boost its temperature, which may be useful for spraying applications.
引用
收藏
页码:2257 / 2265
页数:9
相关论文
共 37 条
[1]  
AARREN G, 1991, 911592 AIAA
[2]   MACH DISK IN UNDEREXPANDED EXHAUST PLUMES [J].
ABBETT, M .
AIAA JOURNAL, 1971, 9 (03) :512-&
[3]  
ABBETT M, 1970, 70231 AIAA
[4]   MULTISCALE TURBULENCE EFFECTS IN UNDEREXPANDED SUPERSONIC JETS [J].
ABDOLHAMID, KS ;
WILMOTH, RG .
AIAA JOURNAL, 1989, 27 (03) :315-322
[5]  
Ashkenas H., 1966, RAREFIED GAS DYN, V2, P84
[6]  
BARTOSIEWICZ Y, 2000, P 8 ANN C CFD CAN CE, V2, P953
[7]   K-ε and Reynolds stress turbulence model comparisons for two-dimensional injection flows [J].
Chenault, CF ;
Beran, PS .
AIAA JOURNAL, 1998, 36 (08) :1401-1412
[8]   Numerical investigation of supersonic injection using a Reynolds-Stress turbulence model [J].
Chenault, CF ;
Beran, PS ;
Bowersox, RDW .
AIAA JOURNAL, 1999, 37 (10) :1257-1269
[9]   PREDICTIONS OF THE STRUCTURE OF TURBULENT, MODERATELY UNDEREXPANDED JETS [J].
CUMBER, PS ;
FAIRWEATHER, M ;
FALLE, SAEG ;
GIDDINGS, JR .
JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 1994, 116 (04) :707-713
[10]  
CUMER P, 1994, J FLUIDS ENG, V117, P599