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contributor authorOh, Seungtaek
contributor authorKim, Jaehyeon
contributor authorKim, Yongmo
date accessioned2019-02-28T10:58:07Z
date available2019-02-28T10:58:07Z
date copyright5/24/2018 12:00:00 AM
date issued2018
identifier issn0742-4795
identifier othergtp_140_09_091501.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4251263
description abstractIn this study, new methodologies are introduced to analyze combustion instability in a lab-scale swirled combustor. First, with the help of radial basis function neural network (RBFNN), the flame describing function (FDF) is effectively modeled from a limited number of experimental data. This neural-network-based FDF method is able to generate more refined FDF data in an extended range. In addition, instead of a perforated plate with round holes, a slotted plate is utilized as a stabilization device. In this approach, the acoustic impedance of a slotted plate is modeled by the Dowling approach, and the dimensions of a slotted plate are optimized by simulated annealing (SA) algorithm to get the highest average absorption coefficient in a given frequency range. The present RBFNN-based FDF approach yields the reasonably good agreements with the measurements in terms of the limit-cycle velocity perturbation ratio and resonant frequency. It is also found that a slotted plate optimized by SA algorithm is quite effective to attenuate combustion instability. Numerical results obtained in this study confirm that these new methodologies are quite reliable and widely applicable for the analysis of combustion instability encountered in practical combustion systems.
publisherThe American Society of Mechanical Engineers (ASME)
titleAnalysis for Combustion Instability and Stabilization Characteristics in a Swirled Premixed Combustor With a Slotted Plate
typeJournal Paper
journal volume140
journal issue9
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4039803
journal fristpage91501
journal lastpage091501-10
treeJournal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 009
contenttypeFulltext


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