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contributor authorMark G. Turner
contributor authorSteven E. Gorrell
contributor authorDavid Car
date accessioned2017-05-09T00:47:24Z
date available2017-05-09T00:47:24Z
date copyrightJuly, 2011
date issued2011
identifier issn0889-504X
identifier otherJOTUEI-28774#031018_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/147804
description abstractThis paper shows a comparison of an unsteady simulation using turbo and an average passage simulation for a two blade row configuration consisting of a wake generator followed by a transonic rotor. Two spacings were simulated, both close and far. The unsteady results compare well with experiment especially for the profile of efficiency difference between close and far. An analysis of results helps to explain the unusual profile seen experimentally that is due to the radial migration of wake generator shed vortices with negative radial velocities near the tip. In addition, different components of the average passage body forces (deterministic stresses) are explored that shows the main terms are the axial momentum and the metal blockage.
publisherThe American Society of Mechanical Engineers (ASME)
titleRadial Migration of Shed Vortices in a Transonic Rotor Following a Wake Generator: A Comparison Between Time Accurate and Average Passage Approaches
typeJournal Paper
journal volume133
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4001241
journal fristpage31018
identifier eissn1528-8900
keywordsWakes
keywordsRotors
keywordsVortices
keywordsGenerators
keywordsBlades
keywordsMomentum
keywordsForce
keywordsMetals
keywordsSimulation
keywordsStress AND Pressure
treeJournal of Turbomachinery:;2011:;volume( 133 ):;issue: 003
contenttypeFulltext


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