2013
DOI: 10.1016/j.ijheatmasstransfer.2012.11.070
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Numerical investigation of pulverized coal jet flame characteristics under different oxy-fuel conditions

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Cited by 18 publications
(9 citation statements)
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“…To overcome the flame stability issue in the oxy‐fuel combustion, they redesigned the burner and increased secondary stream swirl which strengthens the IRZ. Jovanović et al proposed a novel LES model able to handle all possible ignition/combustion mechanism of pulverized coal particles in oxy‐fuel combustion and solved ignited jet flame of pulverized coal using proposed model. They addressed limitations of the standard k‐ε model by comparing the performance of the proposed model with the standard model.…”
Section: Aspects Of Coal Combustionmentioning
confidence: 57%
“…To overcome the flame stability issue in the oxy‐fuel combustion, they redesigned the burner and increased secondary stream swirl which strengthens the IRZ. Jovanović et al proposed a novel LES model able to handle all possible ignition/combustion mechanism of pulverized coal particles in oxy‐fuel combustion and solved ignited jet flame of pulverized coal using proposed model. They addressed limitations of the standard k‐ε model by comparing the performance of the proposed model with the standard model.…”
Section: Aspects Of Coal Combustionmentioning
confidence: 57%
“…For stoichiometric and lean conditions of glycine, the reactions were carried out under oxidizer conditions. Glycine has a small carbonic chain, and the presence of N and OH in the structure provides an intense and fast high-temperature combustion during ignition, which releases a high volume of gases [42]. Smaller crystallites and more porous structures were achieved for these compositions since the entry of oxygen is not a problem.…”
Section: Resultsmentioning
confidence: 99%
“…These properties are mainly adjusted by controlling the chemical composition of the fuel and the ratio of fuel to the oxidizer ratio [41]. The stoichiometry of the SCS reactions is determined based on calculations for fueloxidizer mixtures in the chemistry of propellants [39][40][41], which consider the amount of oxidizing and reducing elements in the reaction [42].…”
Section: Introductionmentioning
confidence: 99%
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“…Because of this reason, the Discrete Ordinates (DO) method was selected for radiation modelling. Weighted sum of gray gases model [4,6] was selected to calculate the fluid absorption coefficient. In addition, scattering function of 0.9, has been used [3].…”
Section: Radiation Modellingmentioning
confidence: 99%