Large Eddy Simulation of an industrial gas turbine combustor using reduced chemistry with accurate pollutant prediction

2017 ◽  
Vol 36 (3) ◽  
pp. 3817-3825 ◽  
Author(s):  
T. Jaravel ◽  
E. Riber ◽  
B. Cuenot ◽  
G. Bulat
2018 ◽  
Vol 34 (5) ◽  
pp. 1269-1284 ◽  
Author(s):  
I. Langella ◽  
Z. X. Chen ◽  
N. Swaminathan ◽  
S. K. Sadasivuni

2005 ◽  
Vol 73 (3) ◽  
pp. 374-381 ◽  
Author(s):  
K. Mahesh ◽  
G. Constantinescu ◽  
S. Apte ◽  
G. Iaccarino ◽  
F. Ham ◽  
...  

Large-eddy simulation (LES) has traditionally been restricted to fairly simple geometries. This paper discusses LES of reacting flows in geometries as complex as commercial gas turbine engine combustors. The incompressible algorithm developed by Mahesh et al. (J. Comput. Phys., 2004, 197, 215–240) is extended to the zero Mach number equations with heat release. Chemical reactions are modeled using the flamelet/progress variable approach of Pierce and Moin (J. Fluid Mech., 2004, 504, 73–97). The simulations are validated against experiment for methane-air combustion in a coaxial geometry, and jet-A surrogate/air combustion in a gas-turbine combustor geometry.


1999 ◽  
Vol 143 (1-6) ◽  
pp. 25-62 ◽  
Author(s):  
WON-WOOK KIM ◽  
SURESH MENON ◽  
HUKAM C. MONGIA

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