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contributor authorS. J. Gallimore
date accessioned2017-05-08T23:23:42Z
date available2017-05-08T23:23:42Z
date copyrightJuly, 1986
date issued1986
identifier issn0889-504X
identifier otherJOTUEI-28577#10_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101848
description abstractThe important influence of spanwise mixing on the flow through multistage axial compressors has been investigated by incorporating the effect into an axisymmetric streamline curvature throughflow program. The mixing was modeled as a turbulent diffusion process based on the experimental observations reported in Part I of this paper, which showed that this was the dominant physical mechanism. The inclusion of the mixing was found to be crucial in accurately predicting spanwise variations of exit total temperature in multistage machines. The effect of mixing on loss distributions inferred from measurements was found to be significant so that upstream loss sources could only be determined from downstream distributions when the effect of mixing was included.
publisherThe American Society of Mechanical Engineers (ASME)
titleSpanwise Mixing in Multistage Axial Flow Compressors: Part II—Throughflow Calculations Including Mixing
typeJournal Paper
journal volume108
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262009
journal fristpage10
journal lastpage16
identifier eissn1528-8900
keywordsCompressors
keywordsAxial flow
keywordsMechanisms
keywordsTurbulent diffusion
keywordsFlow (Dynamics)
keywordsTemperature
keywordsMachinery AND Measurement
treeJournal of Turbomachinery:;1986:;volume( 108 ):;issue: 001
contenttypeFulltext


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