DNS AND LES OF SOOT FORMATION IN OXY-FUEL SPRAY FLAME: APPLICATION OF A NON-ADIABATIC FLAMELET/PROGRESS-VARIABLE APPROACH

2018 ◽  
Author(s):  
Reo Kai ◽  
Akihiro Kishimoto ◽  
Kenichiro Takenaka ◽  
Masaya Muto ◽  
Ryoichi Kurose
2008 ◽  
Vol 612 ◽  
pp. 45-79 ◽  
Author(s):  
YUYA BABA ◽  
RYOICHI KUROSE

The validity of a steady-flamelet model and a flamelet/progress-variable approach for gaseous and spray combustion is investigated by a two-dimensional direct numerical simulation (DNS) of gaseous and spray jet flames, and the combustion characteristics are analysed. A modified flamelet/progress-variable approach, in which total enthalpy rather than product mass fraction is chosen as a progress variable, is also examined. DNS with an Arrhenius formation, in which the chemical reaction is directly solved in the physical flow field, is performed as a reference to validate the combustion models. The results show that the diffusion flame is dominant in the gaseous diffusion jet flame, whereas diffusion and premixed flames coexist in the spray jet flame. The characteristics of the spray flame change from premixed–diffusion coexistent to diffusion-dominant downstream. Comparisons among the results from DNS with various combustion models show the modified flamelet/progress-variable approach to be superior to the other combustion models, particularly for the spray flame. Where the behaviour of the gaseous total enthalpy is strongly affected by the energy transfer (i.e. heat transfer and mass transfer) from the dispersed droplet, and this effect can be accounted for only by solving the conservation equation of the total enthalpy. However, even the DNS with the modified flamelet/progress-variable approach tends to underestimate the gaseous temperature in the central region of the spray jet flame. To increase the prediction accuracy, a combustion model for the partially premixed flame for the spray flame is necessary.


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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