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contributor authorKaralus, Megan
contributor authorThakre, Piyush
contributor authorGoldin, Graham
contributor authorBrandt, Dustin
date accessioned2022-05-08T09:14:52Z
date available2022-05-08T09:14:52Z
date copyright10/12/2021 12:00:00 AM
date issued2021
identifier issn0742-4795
identifier othergtp_144_01_011004.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4284898
description abstractA Honeywell liquid-fueled gas turbine test combustor at idle conditions is numerically investigated in simcenterstar-ccm+ version 2020.3. This work presents large eddy simulation (LES) results using both the flamelet generated manifold (FGM) and detailed chemistry combustion models. Both take advantage of a hybrid chemical (HyChem) mechanism which has previously demonstrated very good accuracy for real fuels such as Jet-A with only 47 species. The objective of this work is to investigate the ability of FGM and detailed chemistry modeling to capture pollutant formation in an aero-engine combustor. Comparisons for NOx, CO, unburned hydrocarbons (UHC), and soot are made, along with the radial temperature profile. To fully capture potential emissions, a soot moment model and Zeldovich NOx model are employed along with radiation. A comparison of results with and without chemistry acceleration techniques for detailed chemistry is included. Then, computational costs are assessed by comparing the performance and scalability of the simulations with each of the combustion models. It is found that the detailed chemistry case with clustering can reproduce nearly identical results to detailed chemistry without any acceleration if CO is added as a clustering variable. With the Lagrangian model settings chosen for this study, the detailed chemistry results compared more favorably with the experimental data than FGM
description abstracthowever, there is uncertainty in the secondary breakup parameters. Sensitivity of the results to a key parameter in the spray breakup model is provided for both FGM and complex chemistry (CC). By varying this breakup rate, the FGM case can predict CO, NOx, and UHC equally well. The smoke number, however, is predicted most accurately by CC. The cost for running detailed chemistry with clustering is found to be about four times that of FGM for this combustor and chemical mechanism.
publisherThe American Society of Mechanical Engineers (ASME)
titleFlamelet Versus Detailed Chemistry Large Eddy Simulation for a Liquid-Fueled Gas Turbine Combustor: A Comparison of Accuracy and Computational Cost
typeJournal Paper
journal volume144
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4052257
journal fristpage11004-1
journal lastpage11004-8
page8
treeJournal of Engineering for Gas Turbines and Power:;2021:;volume( 144 ):;issue: 001
contenttypeFulltext


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