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contributor authorRiأ©ra, William
contributor authorCastillon, Lionel
contributor authorMarty, Julien
contributor authorLeboeuf, Francis
date accessioned2017-05-09T01:13:16Z
date available2017-05-09T01:13:16Z
date issued2014
identifier issn0889-504X
identifier otherturb_136_04_041018.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/156522
description abstractIn the present study, the influence of the inlet condition on the tip clearance flow of an axial compressor is investigated. Two different zonal detached eddy simulations (ZDES) computations are carried out and compared to Reynoldsaveraged Navier–Stokes (RANS) and unsteady RANS (URANS) computations as well as to experimental data. A rotating distortion map of the flow cartography is set as inlet condition for the first ZDES computation. An azimuthally averaged inlet condition is used for the second one and uncouples the rotor tipleakage vortex flutter phenomenon, which stems from the arrival of the inlet guide vane wake from the behavior inherent to the rotor tipleakage vortex. In the studied configuration, the inlet guide vane tip vortex reveals to lower the effects from double leakage on the rotor. The topology of the rotor tipleakage vortex is described, and its development is analyzed.
publisherThe American Society of Mechanical Engineers (ASME)
titleInlet Condition Effects on the Tip Clearance Flow With Zonal Detached Eddy Simulation
typeJournal Paper
journal volume136
journal issue4
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4025216
journal fristpage41018
journal lastpage41018
identifier eissn1528-8900
treeJournal of Turbomachinery:;2014:;volume( 136 ):;issue: 004
contenttypeFulltext


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