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contributor authorA. Pinarbasi
contributor authorM. W. Johnson
date accessioned2017-05-08T23:48:34Z
date available2017-05-08T23:48:34Z
date copyrightOctober, 1995
date issued1995
identifier issn0889-504X
identifier otherJOTUEI-28646#602_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116116
description abstractDetailed measurements have been taken of the three-dimensional velocity field within the vaneless diffuser of a backswept low speed centrifugal compressor using hot-wire anemometry. A 16 percent below and an 11 percent above design flow rate were used in the present study. Results at both flow rates show how the blade wake mixes out more rapidly than the passage wake. Strong secondary flows inherited from the impeller at the higher flow rate delay the mixing out of the circumferential velocity variations, but at both flow rates these circumferential variations are negligible at the last measurement station. The measured tangential/radial flow angle is used to recommend optimum values for the vaneless space and vane angle for design of a vaned diffuser.
publisherThe American Society of Mechanical Engineers (ASME)
titleOff-Design Flow Measurements in a Centrifugal Compressor Vaneless Diffuser
typeJournal Paper
journal volume117
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2836574
journal fristpage602
journal lastpage608
identifier eissn1528-8900
keywordsCompressors
keywordsDesign
keywordsFlow measurement
keywordsVaneless diffusers
keywordsFlow (Dynamics)
keywordsWakes
keywordsDiffusers
keywordsBlades
keywordsDelays
keywordsMeasurement
keywordsWire
keywordsImpellers AND Radial flow
treeJournal of Turbomachinery:;1995:;volume( 117 ):;issue: 004
contenttypeFulltext


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