Global emissions can be significantly reduced with the use of zerocarbon emission fuels. Ammonia is now at the center of attention because of its promise as a carbon-free energy fuel. So, a detailed study on ammonia's combustion and emission characteristics is necessary, especially at low− intermediate temperature and high-pressure conditions. Very few reaction models are available for low−intermediate-temperature ammonia chemistry, and most of them could not show reasonable agreement with the experimental conditions. In the present work, a new ammonia oxidation reaction model has been proposed by referring to the previous available literature for low−intermediate temperature and high-pressure ammonia oxidation chemistry, and also a comprehensive chemical kinetic modeling for the autoignition characteristics and NO x emissions is performed for an ammonia/air mixture using the newly proposed mechanism. The newly proposed ammonia reaction model consists of 32 species and 259 reactions. The proposed mechanism has also been tested by performing the computational fluid dynamics (CFD) modeling for a premixed NH 3 /air mixture in a microflow reactor with varying wall temperature at equivalence ratios of 0.8, 1, and 1.2, and the model validation has been carried out by comparing the mole fraction profiles of species NH 3 , O 2 , and H 2 O with the available experimental results. The proposed reaction model was able to predict the formation of steady weak flames of the NH 3 /air premixed mixture within the computational domain. An excellent agreement is observed between the computational and experimental results for autoignition properties and CFD model validation using the newly proposed reaction model.
The chemical kinetics of methane oxidation in a steam-diluted environment are studied in the present study. Various well-validated mechanisms for methane combustion are adopted and compared with experimental data. Ignition delay, laminar flame speed, and emissions for CH4 combustion with steam dilution are discussed. Cumulative relative error parameter was determined for all mechanisms considered in this study to evaluate the prediction level in quantifiable terms. Reaction pathways under no and steam-diluted environments are analyzed, and key elementary reactions and species are identified in these conditions. The analysis gives a relative idea of the applicability of some of the reduced mechanisms for the diluted steam conditions. This study aims to guide future computational fluid dynamics simulations to accurately predict combustion characteristics in these conditions. Computations of laminar flame speed from GRI-3.0, Aramco3.0, Curran, and San Diego mechanisms were the most precise under diluted steam conditions. Similarly, for the calculation of ignition delay of methane under the steam dilution, the Aramco mechanism and the Curran’s mechanism were able to predict the experimentally observed values most closely. Sensitivity study for the OH concentrations shows that the H-abstraction of methane from OH radicals has an opposing trend with dilution for Aramco and GRI-3.0 mechanism. On the other hand, CO and NO emissions were reduced significantly, with the dilution increased from 0 to 20%. The third-body effect of steam is observed to dominate the deviation observed between the detailed and reduced mechanism. For low operating pressure conditions, the GRI-3.0 mechanism gives an excellent prediction, whereas, for applications like gas turbines and furnaces, Aramco-3.0 and Curran mechanisms can be adopted to give good results. The San Diego mechanism can be chosen for low computational facility purposes as it shows very good predictions for ignition delay and laminar flame speed computations.
This article presents the results of computations on pilot-based turbulent methane/air co-flow diffusion flames under the influence of the preheated oxidizer temperature ranging from 293 to 723 K at two operating pressures of 1 and 3 atm. The focus is on investigating the soot formation and flame structure under the influence of both the preheated air and combustor pressure. The computations were conducted in a 2D axisymmetric computational domain by solving the Favre averaged governing equation using the finite volume-based CFD code Ansys Fluent 19.2. A steady laminar flamelet model in combination with GRI Mech 3.0 was considered for combustion modeling. A semi-empirical acetylene-based soot model proposed by Brookes and Moss was adopted to predict soot. A careful validation was initially carried out with the measurements by Brookes and Moss at 1 and 3 atm with the temperature of both fuel and air at 290 K before carrying out further simulation using preheated air. The results by the present computation demonstrated that the flame peak temperature increased with air temperature for both 1 and 3 atm, while it reduced with pressure elevation. The OH mole fraction, signifying reaction rate, increased with a rise in the oxidizer temperature at the two operating pressures of 1 and 3 atm. However, a reduced value of OH mole fraction was observed at 3 atm when compared with 1 atm. The soot volume fraction increased with air temperature as well as pressure. The reaction rate by soot surface growth, soot mass-nucleation, and soot-oxidation rate increased with an increase in both air temperature and pressure. Finally, the fuel consumption rate showed a decreasing trend with air temperature and an increasing trend with pressure elevation.
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