Title of article :
Numerical Simulation of a Confined Swirling Flow in a Model Gas Turbine Combustor
Author/Authors :
Bazdidi-Tehrani, F. iran university of science and technology - Dept of Mechanical Eng, تهران, ايران , Jahromi, M. iran university of science and technology - Dept of Mechanical Eng, تهران, ايران
From page :
97
To page :
104
Abstract :
The present paper describes a numerical investigation of a confined swirling flow in a model combustion chamber. Two turbulence models, the standard k-e model and the Reynolds stress model (RSM) are employed for the flow predictions. Solutions to the two-dimensional axisymmetric incompressible Reynolds-averaged Navier-Stokes equations have been obtained by the Finite-Volume method. Comparisons of the present numerical predictions with the available experimental data reveal superiority of the RSM over the standard k-e model for prediction of swirling flows. For instance, RSM predicts the central toroidal recirculation zone well, but k-e does not.
Journal title :
Journal of Aerospace Science and Technology (JAST)
Journal title :
Journal of Aerospace Science and Technology (JAST)
Record number :
2747294
Link To Document :
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