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contributor authorLuo, Zibing
contributor authorMa, Zhaokai
contributor authorLi, Jianghua
contributor authorYang, Yong
contributor authorZhang, Jiande
contributor authorLi, Wenkai
contributor authorLiu, Chang
date accessioned2026-08-23T07:22:54Z
date available2026-08-23T07:22:54Z
date copyright2026/08/01
date issued2026
identifier issn0742-4795
identifier othergtp-25-1460.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4315022
description abstractAbstract. The performance of nozzles in the combustor is critical to the combustion process, and carbon deposition on the nozzles can significantly degrade combustion efficiency. Although many studies have been conducted on the spray combustion process under carbon-deposited nozzles, there is still a lack of coupling research on primary atomization and secondary atomization, as well as simulation research on the entire process from atomization to combustion. Therefore, this study first employed a hybrid atomization model combining volume of fluid (VOF) and discrete phase model (DPM), along with delayed detached eddy simulation (DDES) and eddy dissipation (ED), to conduct an unsteady numerical simulation of the entire process from atomization to combustion in the combustor with half of the nozzles blocked by carbon deposits. The results demonstrate that carbon deposits will cause deterioration of atomization and combustion performance: (1) the liquid film thickens and the spray cone angle decreases; (2) at the outlet of the radial swirl, the number of fuel droplets increases while their mean velocity is 21.8% higher than that of the normal nozzles; (3) the temperature distribution at the outlet of the combustor is uneven, with a temperature difference of 218 K. These results provide a feasible basis for exploring the influence of nozzle state on the spray combustion process by using the VOF-DPM hybrid atomization model and the ED model.
publisherThe American Society of Mechanical Engineers (ASME)
titleDelayed Detached Eddy Simulation of Spray Combustion in a Gas Turbine Combustor With and Without Nozzle Blockage
typeJournal Paper
journal volume148
journal issue8
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4070737
journal fristpage488
journal lastpage501
page14
treeJournal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:008
contenttypeFulltext


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