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contributor authorManuj Dhingra
contributor authorAndrew Breeze-Stringfellow
contributor authorHyoun-Woo Shin
contributor authorYedidia Neumeier
contributor authorJ. V. R. Prasad
contributor authorPeter N. Szucs
date accessioned2017-05-09T00:23:38Z
date available2017-05-09T00:23:38Z
date copyrightJuly, 2007
date issued2007
identifier issn1528-8919
identifier otherJETPEZ-26960#730_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/135699
description abstractA stability measure rooted in the unsteady characteristics of the flow field over the compressor rotor has been previously developed. The present work explores the relationship between the stochastic properties of this measure, called the correlation measure, and the compressor stability boundary. A stochastic model has been developed to gauge the impact of the correlation measure’s stochastic nature on its applicability to compressor stability management. The genesis of this model is in the fundamental properties of a specific stochastic process, one that is created by the threshold crossings of a random process. The model validation utilizes data obtained on three different axial compressor facilities. These include a single-stage low-speed axial compressor, a four-stage low-speed research compressor, and an advanced technology demonstrator high-speed compressor. This paper presents details of the model development and validation, as well as closed loop experimental results to demonstrate correlation measure’s usefulness in compressor stability management.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Stochastic Model for a Compressor Stability Measure
typeJournal Paper
journal volume129
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2718231
journal fristpage730
journal lastpage737
identifier eissn0742-4795
keywordsCompressors AND Stability
treeJournal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 003
contenttypeFulltext


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