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contributor authorR. C. Stauter
date accessioned2017-05-08T23:42:51Z
date available2017-05-08T23:42:51Z
date copyrightJuly, 1993
date issued1993
identifier issn0889-504X
identifier otherJOTUEI-28630#468_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112793
description abstractA two-color, five-beam LDV system has been configured to make simultaneous three-component velocity measurements of the flow field in a two-stage axial compressor model. The system has been used to make time-resolved measurements both between compressor blade rows and within the rotating blade passages in an axial compressor. The data show the nature and behavior of the complex, three-dimensional flow phenomena present in the tip region of a compressor as they convect downstream. In particular, the nature of the tip leakage vortex is apparent, being manifested by high blockage as well as the expected vortical motion. The data indicate that the radial flows associated with the tip leakage vortex begin to decrease while within the rotor passage, and that they temporarily increase aft of the passage.
publisherThe American Society of Mechanical Engineers (ASME)
titleMeasurement of the Three-Dimensional Tip Region Flow Field in an Axial Compressor
typeJournal Paper
journal volume115
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2929275
journal fristpage468
journal lastpage476
identifier eissn1528-8900
keywordsFlow (Dynamics)
keywordsCompressors
keywordsVortices
keywordsLeakage
keywordsRotating blades
keywordsLight trucks
keywordsBlades
keywordsRadial flow
keywordsVelocity measurement
keywordsLaser Doppler anemometry
keywordsVortex motion
keywordsRotors AND Measurement
treeJournal of Turbomachinery:;1993:;volume( 115 ):;issue: 003
contenttypeFulltext


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