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contributor authorA. N. Lakshminarasimha
contributor authorM. P. Boyce
contributor authorC. B. Meher-Homji
date accessioned2017-05-08T23:44:14Z
date available2017-05-08T23:44:14Z
date copyrightJanuary, 1994
date issued1994
identifier issn1528-8919
identifier otherJETPEZ-26722#46_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113604
description abstractThe effects of performance deterioration in both land and aircraft gas turbines are presented in this paper. Models for two of the most common causes of deterioration, viz., fouling and erosion, are presented. A stage-stacking procedure, which uses new installed engine field data for compressor map development, is described. The results of the effect of fouling in a powerplant gas turbine and that of erosion in a aircraft gas turbine are presented. Also described are methods of fault threshold quantification and fault matrix simulation. Results of the analyses were found to be consistent with field observations.
publisherThe American Society of Mechanical Engineers (ASME)
titleModeling and Analysis of Gas Turbine Performance Deterioration
typeJournal Paper
journal volume116
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2906808
journal fristpage46
journal lastpage52
identifier eissn0742-4795
keywordsGas turbines
keywordsModeling
keywordsErosion
keywordsAircraft
keywordsPower stations
keywordsEngines
keywordsCompressors AND Simulation
treeJournal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 001
contenttypeFulltext


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