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contributor authorMichelassi, Vittorio
contributor authorChen, Li
contributor authorPichler, Richard
contributor authorSandberg, Richard D.
date accessioned2017-05-09T01:24:37Z
date available2017-05-09T01:24:37Z
date issued2015
identifier issn0889-504X
identifier otherturbo_137_07_071005.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159941
description abstractIn the present paper, direct numerical simulation (DNS) studies of the compressible flow in the T106 linear cascade have been carried out. Various environmental variables, i.e., background turbulence level, frequency of incoming wakes, and Reynolds number, and a combination of these were considered for a total of 12 fully resolved simulations. The mechanisms dictating the observed flow phenomena, including the mixing and distortion of the incoming wakes, wake/boundary layer interaction, and boundary layer evolution impact on profile loss generation, are studied systematically. A detailed loss generation analysis allows the identification of each source of loss in boundary layers and flow core. Particular attention is devoted to the concerted impact of wakes distortion mechanics and the intermittent nature of the unsteady boundary layer. Further, the present study examines the validity of the Boussinesq eddy viscosity assumption, which invokes a linear stress–strain relationship in commonly used RANS models. The errors originating from this assumption are scrutinized with both time and phaselocked averaged flow fields to possibly identify shortcomings of traditional RANS models.
publisherThe American Society of Mechanical Engineers (ASME)
titleCompressible Direct Numerical Simulation of Low Pressure Turbines—Part II: Effect of Inflow Disturbances
typeJournal Paper
journal volume137
journal issue7
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4029126
journal fristpage71005
journal lastpage71005
identifier eissn1528-8900
treeJournal of Turbomachinery:;2015:;volume( 137 ):;issue: 007
contenttypeFulltext


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