Modelling compressible gas flow near the nozzle of a gas atomiser using a new unified model

被引:16
作者
Tong, Mingming [1 ]
Browne, David J. [1 ]
机构
[1] Natl Univ Ireland Univ Coll Dublin, Sch Elect Elect & Mech Engn, Ctr Mat Sci & Engn, Dublin 4, Ireland
关键词
CLOSE-COUPLED NOZZLES; FRONT-TRACKING MODEL; BOUNDARY-CONDITIONS; INCOMPRESSIBLE FLOWS; DIRECT COMPUTATION; FLUID-DYNAMICS; FREE SURFACES; ATOMIZATION; MELT; FORMULATION;
D O I
10.1016/j.compfluid.2008.11.014
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
In this paper, a unified numerical model is used to simulate the compressible gas flow, during the process of atomisation of liquid, near the atomiser nozzle in gas-only case studies. The flow of the under-expanded gas jets is studied, by analyzing the pressure field, density field and the spatial distribution of Mach number of the gas. The simulated predictions of gas status at the nozzle exit, the radial profile of Pitot pressure, aspiration pressure, and the spatial distribution of the density gradient, are compared with relevant experimental results and an analytical correlation. in order to validate and verify the application of this unified model in the numerical simulation of the gas dynamic behavior during gas atomisation. The simulation results show that the compressible gas flow near the nozzle of a discrete jet atomiser is different from that in a typical annular slit atomiser. Unlike existing models, this new formulation has the potential to be used in future to simulate the simultaneous flow of compressible gas and a weakly compressible liquid metal stream. (C) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1183 / 1190
页数:8
相关论文
共 45 条
[1]   Modelling columnar dendritic growth into an undercooled metallic melt in the presence of convection [J].
Banaszek, J ;
Browne, DJ .
MATERIALS TRANSACTIONS, 2005, 46 (06) :1378-1387
[2]  
BIJI H, 1998, J COMPUT PHYS, V141, P153
[3]  
BROWN SG, 2007, D86 IMPRESS ESTEC, P56
[4]  
Browne D. J., 2003, Archives of Thermodynamics, V24, P25
[5]   A fixed grid front-tracking model of the growth of a columnar front and an equiaxed grain during solidification of an alloy [J].
Browne, DJ ;
Hunt, JD .
NUMERICAL HEAT TRANSFER PART B-FUNDAMENTALS, 2004, 45 (05) :395-419
[6]  
COLLIS SS, 19960180 AM I AER AS
[7]   BOUNDARY-CONDITIONS FOR DIRECT COMPUTATION OF AERODYNAMIC SOUND GENERATION [J].
COLONIUS, T ;
LELE, SK ;
MOIN, P .
AIAA JOURNAL, 1993, 31 (09) :1574-1582
[8]   Proposed inflow/outflow boundary condition for direct computation of aerodynamic sound [J].
Freund, JB .
AIAA JOURNAL, 1997, 35 (04) :740-742
[9]  
FRITSCHING U, 1992, PHOENICS J COMPUT FL, V5, P81
[10]   On the behaviour of upwind schemes in the low Mach number limit [J].
Guillard, H ;
Viozat, C .
COMPUTERS & FLUIDS, 1999, 28 (01) :63-86