Solutions for a turbulent jet diffusion flame of ethanol with NOx formation using a reduced kinetic mechanism obtained by applying ANNs

Fuel ◽  
2018 ◽  
Vol 231 ◽  
pp. 373-378 ◽  
Author(s):  
F.N. Pereira ◽  
A.L. De Bortoli
Author(s):  
N. K. Rizk ◽  
H. C. Mongia

A recently developed emission model was used to predict the emission characteristics of a gas turbine combustor. The model involves a multiple-step reaction scheme that addresses the breakup of the fuel into an intermediate hydrocarbon compound of variable structure. The reaction rate expressions developed in the present approach simulated the results obtained using a detailed chemical kinetic mechanism over a wide range of operation that is typically encountered in a conventional diffusion flame combustor, as well as low NOx rich/quench/lean, and premixed/prevaporized lean combustion concepts. The modeling of the combustor involves dividing the combustor into a number of reactors representing various combustion and near wall regions of the combustor. The calculations showed that the fuel reaction could proceed at a completely different rate depending on the conditions prevailing in each region of the combustor. The model results also indicated that at idle power mode the initial rate of NOx formation was high. However, due to the subsequent admission of air, no further addition to the NOx concentration was predicted at downstream locations. At high power levels, the fuel rich region near the combustor dome inhibits the formation of NOx. The admission of air in this case brings the fuel/air mixture close to the stoichiometric value causing a significant amount of NOx to form. The model calculations agreed quite well with the measured data of the combustor.


2012 ◽  
Vol 11 (1-2) ◽  
pp. 37
Author(s):  
G. S. L. Andreis ◽  
R. S. Gomes ◽  
A. L. De Bortoli

Propane is one of the simplest hydrocarbons that can be a representative of higher hydrocarbons used in many applications. Therefore, this work develops a ten-step reduced kinetic mechanism among 14 reactive species for the propane combustion. The model is based on the solution of the flamelet equations. The equations are discretized using the second-order space finite difference method, using LES (Large-Eddy Simulation). Obtained results compare favorably with data in the literature for a propane jet diffusion flame. The main advantage of this strategy is the decrease of the work needed to solve the system of governing equations.


2018 ◽  
Vol 32 (1) ◽  
pp. 867-874 ◽  
Author(s):  
Mario Díaz-González ◽  
Cesar Treviño ◽  
Juan C. Prince

2012 ◽  
Vol 48 (5) ◽  
pp. 590-601 ◽  
Author(s):  
T. A. Bol’shova ◽  
A. G. Shmakov ◽  
S. A. Yakimov ◽  
D. A. Knyaz’kov ◽  
O. P. Korobeinichev

Author(s):  
Beijing Zhong ◽  
Shuai Dang ◽  
Jun Xi

In this study, numerical simulations for an n-heptane fueled Chaochai 6102bzl direct injection diesel engine are performed in order to predict the chemical details of the combustion process and resulting polycyclic aromatic hydrocarbons (such as benzene, naphthalene, phenanthrene and pyrene) formation. The diesel geometry and reduced kinetic mechanism of n-heptane oxidation, which includes only 86 reactions and 57 species, have been developed and incorporated into the computational fluid dynamics code, FLUENT. The diesel unsteady laminar flamelet model, turbulence model and spray model have been employed in the numerical simulations. The numerical simulation results showed that the polycyclic aromatic hydrocarbons were firstly increased with the increase of diesel crank angel and then decreased, which was mostly located at the bottom of diesel combustion chamber wall.


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