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contributor authorBeni Cukurel
contributor authorPatrick B. Lawless
contributor authorSanford Fleeter
date accessioned2017-05-09T00:41:36Z
date available2017-05-09T00:41:36Z
date copyrightApril, 2010
date issued2010
identifier issn0889-504X
identifier otherJOTUEI-28762#021010_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/145016
description abstractAn efficient diffuser is essential to a modern compressor stage due to its significance in stage performance, durability, and operability. To address the need for data that describe the complex, unsteady flow field in a vaned diffuser, particle image velocity is utilized to characterize the spanwise and circumferential variations in the flow features in the vaned diffuser passage of a transonic centrifugal compressor. The spanwise variation in the diffuser flow field is further investigated by the comparison of three different operating conditions representative of low, nominal, and high loading. These data demonstrate that not only the diffuser flow field is highly dependent on the operation conditions, e.g., hub-to-shroud variation increases with loading, but also the circumferential periodicity, created by the highly three dimensional impeller discharge flow, generates a larger unsteadiness toward the hub region of the vaned diffuser.
publisherThe American Society of Mechanical Engineers (ASME)
titleParticle Image Velocity Investigation of a High Speed Centrifugal Compressor Diffuser: Spanwise and Loading Variations
typeJournal Paper
journal volume132
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3104616
journal fristpage21010
identifier eissn1528-8900
keywordsFlow (Dynamics)
keywordsCompressors
keywordsImpellers
keywordsDiffusers
keywordsParticulate matter AND Mach number
treeJournal of Turbomachinery:;2010:;volume( 132 ):;issue: 002
contenttypeFulltext


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