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

2004 ◽  
Author(s):  
R. Steiner ◽  
C. Bauer ◽  
C. Krüger ◽  
F. Otto ◽  
U. Maas
Keyword(s):  
3D Simulation ◽  
Diesel Combustion ◽  
Progress Variable ◽  
Variable Approach ◽  
Complex Chemistry

Large eddy simulation with flamelet progress variable approach combined with artificial neural network acceleration

2021 ◽  
Author(s):  
Lorenzo Angelilli ◽  
Pietro Paolo Ciottoli ◽  
Riccardo Malpica Galassi ◽  
Francisco E. Hernandez Perez ◽  
Mattia Soldan ◽  
...  
Keyword(s):  
Neural Network ◽  
Artificial Neural Network ◽  
Large Eddy Simulation ◽  
Progress Variable ◽  
Eddy Simulation ◽  
Variable Approach ◽  
Large Eddy ◽  
Artificial Neural

scholarly journals An SMLD Joint PDF Model for Turbulent Non-Premixed Combustion Using the Flamelet Progress-Variable Approach

2015 ◽  
Vol 95 (1) ◽  
pp. 97-119 ◽  
Author(s):  
Alessandro Coclite ◽  
Giuseppe Pascazio ◽  
Pietro De Palma ◽  
Luigi Cutrone ◽  
Matthias Ihme
Keyword(s):  
Premixed Combustion ◽  
Progress Variable ◽  
Variable Approach ◽  
Pdf Model

scholarly journals Unsteady flamelet/progress variable approach for non-premixed turbulent lifted flames

2010 ◽  
Vol 4 (3) ◽  
pp. 465-474 ◽  
Author(s):  
S. K. Sadasivuni ◽  
W. Malalasekera ◽  
S. S. Ibrahim
Keyword(s):  
Progress Variable ◽  
Variable Approach ◽  
Lifted Flames

Large-Eddy Simulation of Reacting Turbulent Flows in Complex Geometries

2005 ◽  
Vol 73 (3) ◽  
pp. 374-381 ◽  
Author(s):  
K. Mahesh ◽  
G. Constantinescu ◽  
S. Apte ◽  
G. Iaccarino ◽  
F. Ham ◽  
...  
Keyword(s):  
Large Eddy Simulation ◽  
Gas Turbine ◽  
Turbulent Flows ◽  
Reacting Flows ◽  
Gas Turbine Combustor ◽  
Turbine Engine ◽  
Progress Variable ◽  
Eddy Simulation ◽  
Variable Approach ◽  
Large Eddy

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.

Sign in / Sign up

Export Citation Format

Share Document