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contributor authorJ. A. Powell
contributor authorA. J. Strazisar
contributor authorR. G. Seasholtz
date accessioned2017-05-08T23:11:08Z
date available2017-05-08T23:11:08Z
date copyrightApril, 1981
date issued1981
identifier issn1528-8919
identifier otherJETPEZ-26765#424_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94541
description abstractInnovative features of the anemometer include: (1) a rapid and efficient data acquisition process, (2) a detailed real-time graphic display of the data being accumulated, and (3) input laser beam positioning that maximizes the size of the intra-rotor region being mapped. Results are presented that demonstrate the anemometer’s capability in flow mapping within a transonic axial-flow compressor rotor. Typically, a velocity profile, derived from 30,000 measurements along 1000 sequential circumferential positions covering 20 blade passages, can be obtained in 30 s. The use of fluorescent seed particles allows flow measurements near the rotor hub and the casing window.
publisherThe American Society of Mechanical Engineers (ASME)
titleEfficient Laser Anemometer for Intra-Rotor Flow Mapping in Turbomachinery
typeJournal Paper
journal volume103
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3230737
journal fristpage424
journal lastpage429
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsLasers
keywordsRotors
keywordsTurbomachinery
keywordsData acquisition
keywordsAxial flow
keywordsBlades
keywordsFlow measurement
keywordsMeasurement
keywordsParticulate matter
keywordsCompressors AND Laser beams
treeJournal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 002
contenttypeFulltext


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