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contributor authorS. Sarkar
contributor authorPeter R. Voke
date accessioned2017-05-09T00:21:58Z
date available2017-05-09T00:21:58Z
date copyrightApril, 2006
date issued2006
identifier issn0889-504X
identifier otherJOTUEI-28728#221_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/134839
description abstractThe unsteady pressure over the suction surface of a modern low-pressure (LP) turbine blade subjected to periodically passing wakes from a moving bar wake generator is described. The results presented are a part of detailed large-eddy simulation (LES) following earlier experiments over the T106 profile for a Reynolds number of 1.6×105 (based on the chord and exit velocity) and the cascade pitch to chord ratio of 0.8. The present LES uses coupled simulations of cylinder for wake, providing four-dimensional inflow conditions for successor simulations of wake interactions with the blade. The three-dimensional, time-dependent, incompressible Navier-Stokes equations in fully covariant form are solved with 2.4×106 grid points for the cascade and 3.05×106 grid points for the cylinder using a symmetry-preserving finite difference scheme of second-order spatial and temporal accuracy. A separation bubble on the suction surface of the blade was found to form under the steady state condition. Pressure fluctuations of large amplitude appear on the suction surface as the wake passes over the separation region. Enhanced receptivity of perturbations associated with the inflexional velocity profile is the cause of instability and coherent vortices appear over the rear half of the suction surface by the rollup of shear layer via Kelvin-Helmholtz (KH) mechanism. Once these vortices are formed, the steady-flow separation changes remarkably. These coherent structures embedded in the boundary layer amplify before breakdown while traveling downstream with a convective speed of about 37% of the local free-stream speed. The vortices play an important role in the generation of turbulence and thus to decide the transitional length, which becomes time dependent. The source of the pressure fluctuations on the rear part of the suction surface is also identified as the formation of these coherent structures. When compared with experiments, it reveals that LES is worth pursuing as an understanding of the eddy motions and interactions is of vital importance for the problem.
publisherThe American Society of Mechanical Engineers (ASME)
titleLarge-Eddy Simulation of Unsteady Surface Pressure Over a Low-Pressure Turbine Blade due to Interactions of Passing Wakes and Inflexional Boundary Layer
typeJournal Paper
journal volume128
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2137741
journal fristpage221
journal lastpage231
identifier eissn1528-8900
keywordsTurbulence
keywordsEddies (Fluid dynamics)
keywordsSuction
keywordsTurbine blades
keywordsPressure
keywordsFlow (Dynamics)
keywordsWakes
keywordsBoundary layers
keywordsBlades
keywordsBubbles
keywordsSeparation (Technology)
keywordsVortices
keywordsFluctuations (Physics) AND Shear (Mechanics)
treeJournal of Turbomachinery:;2006:;volume( 128 ):;issue: 002
contenttypeFulltext


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