3D-CFD Simulation of DI-Diesel Combustion Applying a Progress Variable Approach Accounting for Detailed Chemistry

Author(s):  
P. Wenzel ◽  
R. Steiner ◽  
C. Krüger ◽  
R. Schießl ◽  
C. Hofrath ◽  
...  
2006 ◽  
Vol 178 (10-11) ◽  
pp. 1977-1997 ◽  
Author(s):  
HARRY LEHTINIEMI ◽  
FABIAN MAUSS ◽  
MICHAEL BALTHASAR ◽  
INGEMAR MAGNUSSON

2021 ◽  
Author(s):  
Lorenzo Angelilli ◽  
Pietro Paolo Ciottoli ◽  
Riccardo Malpica Galassi ◽  
Francisco E. Hernandez Perez ◽  
Mattia Soldan ◽  
...  

2015 ◽  
Vol 95 (1) ◽  
pp. 97-119 ◽  
Author(s):  
Alessandro Coclite ◽  
Giuseppe Pascazio ◽  
Pietro De Palma ◽  
Luigi Cutrone ◽  
Matthias Ihme

2010 ◽  
Vol 4 (3) ◽  
pp. 465-474 ◽  
Author(s):  
S. K. Sadasivuni ◽  
W. Malalasekera ◽  
S. S. Ibrahim

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.


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