Probing into the effects of fuel injection pressure and nozzle hole diameter on spray characteristics under ultra-high injection pressures using advanced breakup model

被引:2
|
作者
Yousefifard, M. [1 ]
Ghadimi, P. [1 ]
Mirsalim, S. M. [2 ]
机构
[1] Amirkabir Univ Technol, Dept Marine Technol, Tehran, Iran
[2] Amirkabir Univ Technol, Dept Mech Engn, Tehran, Iran
关键词
Diesel spray; Ultra-high injection pressure; Nozzle hole diameter; Penetration length; Breakup model; OpenFOAM; DIESEL; ATOMIZATION; PENETRATION; ENGINE; GEOMETRY;
D O I
10.24200/sci.2016.3829
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this article, non-evaporating and non-reacting diesel spray is modeled under ultra-high injection pressure using an Eulerian-Lagrangian scheme. This is accomplished in order to probe into the effects of injection pressure, nozzle diameter, and ambient density on spray characteristics. An advanced hybrid breakup model that takes into consideration the transient processes during spray injection has been added to the open source code, OpenFOAM. Reynolds-Average Navier-Stokes (RANS) equations are solved using the standard k - epsilon turbulence model and the fuel droplet is tracked by a Lagrangian scheme. Published experimental data have been used for validation of spray characteristics at 15 kg/m(3) ambient density and injection pressures of 100, 200 and 300 MPa. Also, three nozzle diameters of 0.08, 0.12 and 0.16 mm have been implemented for investigating the effect of this parameter on spray formation. Computed spray shape, jet penetration, spray volume, equivalent ratio along the injector axis and Sauter Mean Diameter (SMD) illustrate good agreement with experimental data of a single hole nozzle and symmetric spray. The effects of fuel injection pressure, nozzle hole diameter and ambient density on main spray parameters are presented. It is concluded that the numerical model presented here is quite suitable for accurately predicting diesel spray shapes under ultra-high injection pressures. (C) 2016 Sharif University of Technology. All rights reserved.
引用
收藏
页码:238 / 248
页数:11
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