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contributor authorD. Bouris
contributor authorR. Kubo
contributor authorH. Hirata
contributor authorY. Nakata
date accessioned2017-05-09T00:07:27Z
date available2017-05-09T00:07:27Z
date copyrightJuly, 2002
date issued2002
identifier issn1528-8919
identifier otherJETPEZ-26814#608_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126750
description abstractCompressor fouling is generally accepted to be an important factor when monitoring the efficiency of an engine’s operation. However, there are not many studies related to the local fouling behavior of the individual components of the compressor. In the present paper, the CFD-ACE software package is used for the flow field calculation and the results are utilized to calculate the deposition rates on the blade surfaces of a conventional compressor stator and rotor. The deposition model takes into account the particle and surface material properties and the energy balance at the point of impact. A discussion is presented regarding the various mechanisms that produce the final deposition rate distribution and how the flow field and blade geometry affect it.
publisherThe American Society of Mechanical Engineers (ASME)
titleNumerical Comparative Study of Compressor Rotor and Stator Blade Deposition Rates
typeJournal Paper
journal volume124
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1454113
journal fristpage608
journal lastpage616
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsParticulate matter
keywordsCompressors
keywordsRotors
keywordsBlades
keywordsStators
keywordsMechanisms
keywordsPressure AND Materials properties
treeJournal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 003
contenttypeFulltext


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