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contributor authorS. Elfeki
contributor authorW. Tabakoff
date accessioned2017-05-08T23:26:06Z
date available2017-05-08T23:26:06Z
date copyrightJanuary, 1987
date issued1987
identifier issn0889-504X
identifier otherJOTUEI-28581#62_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103265
description abstractGas turbine engines operating in areas where the atmosphere is polluted by small solid particles are examples of machines operating under particulate two-phase flow conditions. The presence of solid particles in the working media leads to erosion and loss of engine power. In the present paper, particle trajectories are calculated by direct integration of the particle equations of motion through a compressor impeller with two different size splitters. Particle collisions with the blade, hub, and casing surfaces are determined. Erosion caused by the particle collisions with the compressor surfaces is calculated.
publisherThe American Society of Mechanical Engineers (ASME)
titleErosion Study of Radial Flow Compressor With Splitters
typeJournal Paper
journal volume109
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262071
journal fristpage62
journal lastpage69
identifier eissn1528-8900
treeJournal of Turbomachinery:;1987:;volume( 109 ):;issue: 001
contenttypeFulltext


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