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contributor authorMeng, Sheng
contributor authorZhou, Hao
contributor authorCen, Kefa
date accessioned2019-09-18T09:02:20Z
date available2019-09-18T09:02:20Z
date copyright6/5/2019 12:00:00 AM
date issued2019
identifier issn0742-4795
identifier othergtp_141_09_091007
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4258140
description abstractPerforated plates are widely used to attenuate noise emission and as acoustic liners in combustion chambers. In this study, the damping performance of the perforated plate located in the combustor inlet section is experimentally and numerically studied. The primary response of nonpremixed swirl flame under 30–400 Hz acoustic excitation with a 445 mm inlet length occurs at 134 Hz and 210 Hz modes. The perforated plate designed for 210 Hz sound absorption with a 328 mm cavity length and an 8.04% porosity is compared to plates with various cavity lengths and different orifice patterns. The acoustic absorption capability of perforated plates is evaluated by the Luong model and tested in an impedance tube. The acoustic measurements show that the sound absorption performance of each plate is strongly affected by the bias flow velocity and cavity length. The combustion results indicate that the installation of perforated plates at the inlet section has two effects: sound attenuation and redistribution of the pressure mode of the combustor. The acoustic mode analysis further demonstrated that, for damping the nonpremixed flame when the combustion instability is caused by the inlet pressure fluctuation, modification of the inlet acoustic mode shape is more efficient than the sound attenuation.
publisherAmerican Society of Mechanical Engineers (ASME)
titleApplication of the Perforated Plate in Passive Control of the Nonpremixed Swirl Combustion Instability Under Acoustic Excitation
typeJournal Paper
journal volume141
journal issue9
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4043848
journal fristpage91007
journal lastpage091007-12
treeJournal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 009
contenttypeFulltext


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