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Comparative Study of Turbulence Modeling in variable<br />
density Jets and Diffusion Flames<br />
F. Tabet-Helal a, B. Sarh a and I. Gökalp a<br />
In this study, the performances of the Reynolds Stress model (RSM) and the<br />
k- model with Pope correction in their turbulence dissipation rate equation, ,<br />
are investigated in many configurations of variable density jet and nonpremixed<br />
flames. The predictions are compared to the available experimental<br />
data.<br />
It is known that the k- model and the RSM model over-predict the<br />
spreading and decay rate of the round jet flow by 40 % 1. To improve the<br />
accuracy of these turbulence models for solving round jet flows and jet flames,<br />
the turbulence constants (C1 and C2) of the turbulence dissipation rate<br />
transport equation may be modified, as they are responsible for the<br />
generation/destruction of the turbulence energy dissipation. Modifications to<br />
the turbulence constants have been suggest in the past by McGuirk and Rodi 2,<br />
Morse 3, Launder et al. 4 and Pope 1. All modifications involve the turbulence<br />
constants becoming functions of the velocity decay rate and jet width. For<br />
complex flows, a more convenient way is to introduce a correction like that<br />
proposed by Pope 1 taking into account the vortex stretching. Also, this<br />
modification is more generally applicable.<br />
The variable density jets studied are respectively methane, air and CO2. The<br />
corresponding density ratio between the jet flow and the air coflow are<br />
respectively 1.8, 1 and 0.66. The diffusion flames considered are respectively,<br />
H2/Air, CH4/Air and CH4-H2-N2/Air flames. A flamelet library approach has<br />
been applied to account for chemistry and turbulence interaction effects. This<br />
work is focused on the applicability of Pope correction to a wide range of<br />
variable density jets and diffusion flames.<br />
A Pope correction model is implemented in the commercial CFD code<br />
Fluent 6.1.22. User-define subroutine function of the flow variables is written<br />
for this purpose.<br />
The results obtained compare favourably with the experimental data. The<br />
two turbulence models predictions including Pope correction in equation are,<br />
in general, very close in all the configurations considered. However, the RSM<br />
model calculations needs more refine mesh and consequently more computing<br />
time than the k- model.<br />
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a LCSR-CNRS, 1 C avenue de la recherché scientifique, Orléans 45071, France.<br />
1 Pope, AIAA J. 16, 3 (1978).<br />
2 Mcguirk and Rodi, 1 st Symp. On Turbulent Shear Flows,71-83, (1979)<br />
3 Morse, PhD Thesis, London University, 1977.<br />
4 Launder et al., NASA SP-311, 1972.<br />
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