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contributor authorSmith, Natalie R.
contributor authorBerdanier, Reid A.
contributor authorFabian, John C.
contributor authorKey, Nicole L.
date accessioned2017-05-09T01:18:28Z
date available2017-05-09T01:18:28Z
date issued2015
identifier issn1528-8919
identifier othergtp_137_12_122603.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/158111
description abstractCareful experimental measurements can capture small changes in compressor total pressure ratio (TPR), which arise with subtle changes in an experiment's configuration. Research facilities that use unconditioned atmospheric air must account for changes in ambient compressor inlet conditions to establish repeatable performance maps. A unique dataset from a threestage axial compressor has been acquired over the duration of 12 months in the Midwest U.S., where ambient conditions change significantly. The trends show a difference in compressor TPR measured on a cold day versus a warm day despite correcting inlet conditions to sea level standard day. To reconcile these differences, this paper explores correcting the compressor exit thermodynamic state, Reynolds number effects, and variations in rotor tip clearance (TC) as a result of differences in thermal growth.
publisherThe American Society of Mechanical Engineers (ASME)
titleReconciling Compressor Performance Differences for Varying Ambient Inlet Conditions
typeJournal Paper
journal volume137
journal issue12
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4030518
journal fristpage122603
journal lastpage122603
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2015:;volume( 137 ):;issue: 012
contenttypeFulltext


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