2021
DOI: 10.1115/1.0003068v
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Numerical Modeling of Gaseous Partially Premixed Low-Swirl Lifted Flame at Elevated Pressure

Abstract: Lifted flames have been investigated in the past years for their benefits in terms of NOx emissions reduction for gas turbine applications. In a lifted flame, the flame front stabilized on a position that is significantly detached from the nozzle exit, improving the premixing process before the reaction zone. The distance between the flame front and the nozzle exit is called liftoff height and it represents the main parameter that characterize this type of flame. In the present work, a partially premixed lifte… Show more

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Cited by 3 publications
(17 citation statements)
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“…Still considering the previous analysis, the main reaction zones again appear at the side of the swirling jet, but a not trivial behaviour is present con- cerning the most reactive side. Although the limits pointed out in the previous paragraph concerning the position of these zones, it could be concluded that these regions are related to the outer shear layer between swirling jet and ORZ, as already pointed out in the previous studies for this type of flame on the single sector both experimentally [15] and numerically [28]. This fact could be observed from the axial velocity maps, where the black isolines identify the production formation rate.…”
Section: Tilt Angle Effectsmentioning
confidence: 49%
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“…Still considering the previous analysis, the main reaction zones again appear at the side of the swirling jet, but a not trivial behaviour is present con- cerning the most reactive side. Although the limits pointed out in the previous paragraph concerning the position of these zones, it could be concluded that these regions are related to the outer shear layer between swirling jet and ORZ, as already pointed out in the previous studies for this type of flame on the single sector both experimentally [15] and numerically [28]. This fact could be observed from the axial velocity maps, where the black isolines identify the production formation rate.…”
Section: Tilt Angle Effectsmentioning
confidence: 49%
“…3 (inner and outlet inlets), a target mass flow rate corresponding to the conditions of Tab.1 has been imposed. This boundary condition consists of an adapted radial profile derived from previously Large Eddy Simulations (LES) carried out on the same nozzle with a smaller effective area [28]. Here, it is assumed that the trend in the radial direction concerning mass flow distribution and turbulent quantities are the same for the two nozzles.…”
Section: Spray Distributionmentioning
confidence: 99%
“…In the previous works by the authors, the effects of heat losses were included within the FGM model through a correction factor applied by scaling the reaction rate [17,18]: outcomes have shown a discrepancy with the experimental measurements, resulting in a short flame stabilized low in the flame tube. A possible explanation for such behaviour could be incorrect modelling of the heat loss effects on the reaction, due to this simplistic approach, as described in [35].…”
Section: Non Adiabatic Flamelet Generated Manifold (Nfgm)mentioning
confidence: 99%
“…On the other hand, the limitations of a priori regime assumption and chemistry tabulation could strongly impact the final prediction [13], and nowadays many research efforts are devoted to compare finite rate methods with and flamelets-based ones for describing turbulent combustion [14,15]. Considering the numerical works carried out so far on the KIT-EBI's flame [16,17], turbulent combustion has been initially modeled with flamelets based approaches as (or very similar to) the Flamelet Generated Manifold (FGM). This model however has shown to overpredict the reaction rate, leading to a flame stabilized too low and short with respect to the experimental finding.…”
Section: Introductionmentioning
confidence: 99%
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