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contributor authorT. R. Camp
contributor authorH.-W. Shin
date accessioned2017-05-08T23:48:39Z
date available2017-05-08T23:48:39Z
date copyrightJanuary, 1995
date issued1995
identifier issn0889-504X
identifier otherJOTUEI-28642#38_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116170
description abstractThis paper describes the measurement and processing of turbulence data from multistage low-speed compressors. Measurements were made at the same relative positions in three four-stage compressors, each having different levels of the design stage loading coefficient. A new method of data processing to calculate turbulence intensities and integral length scales is outlined. Using this method, integral length scales have been measured in turbomachinery flows for the first time. It is shown how the turbulence intensity and integral length scale vary with position in the blade passage, with changing flow coefficient and with the value of the design stage loading coefficient. The results have been used to specify representative inlet conditions for experimental rigs and to improve the application of CFD turbulence models to turbomachinery modeling.
publisherThe American Society of Mechanical Engineers (ASME)
titleTurbulence Intensity and Length Scale Measurements in Multistage Compressors
typeJournal Paper
journal volume117
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2835642
journal fristpage38
journal lastpage46
identifier eissn1528-8900
keywordsMeasurement
keywordsTurbulence
keywordsCompressors
keywordsDesign
keywordsFlow (Dynamics)
keywordsTurbomachinery
keywordsModeling
keywordsBlades AND Computational fluid dynamics
treeJournal of Turbomachinery:;1995:;volume( 117 ):;issue: 001
contenttypeFulltext


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