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contributor authorJ. J. Adamczyk
contributor authorM. L. Celestina
contributor authorM. Barnett
contributor authorT. A. Beach
date accessioned2017-05-08T23:34:05Z
date available2017-05-08T23:34:05Z
date copyrightJuly, 1990
date issued1990
identifier issn0889-504X
identifier otherJOTUEI-28604#370_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107721
description abstractThis work outlines a procedure for simulating the flow field within multistage turbomachinery, which includes the effects of unsteadiness, compressibility, and viscosity. The associated modeling equations are the average passage equation system, which governs the time-averaged flow field within a typical passage of a blade row embedded within a multistage configuration. The results from a simulation of a low aspect ratio stage and one-half turbine will be presented and compared with experimental measurements. It will be shown that the secondary flow field generated by the rotor causes the aerodynamic performance of the downstream vane to be significantly different from that of an isolated blade row.
publisherThe American Society of Mechanical Engineers (ASME)
titleSimulation of Three-Dimensional Viscous Flow Within a Multistage Turbine
typeJournal Paper
journal volume112
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2927669
journal fristpage370
journal lastpage376
identifier eissn1528-8900
keywordsSimulation
keywordsViscous flow
keywordsTurbines
keywordsFlow (Dynamics)
keywordsBlades
keywordsEquations
keywordsTurbomachinery
keywordsModeling
keywordsRotors
keywordsMeasurement
keywordsViscosity AND Compressibility
treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 003
contenttypeFulltext


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