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contributor authorF. E. Ames
contributor authorM. W. Plesniak
date accessioned2017-05-08T23:55:09Z
date available2017-05-08T23:55:09Z
date copyrightApril, 1997
date issued1997
identifier issn0889-504X
identifier otherJOTUEI-28659#182_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119624
description abstractAn experimental research program was undertaken to examine the influence of large-scale high-intensity turbulence on vane exit losses, wake growth, and exit turbulence characteristics. The experiment was conducted in a four-vane linear cascade at an exit Reynolds number of 800,000 based on chord length and an exit Mach number of 0.27. Exit measurements were made for four inlet turbulence conditions including a low-turbulence case (Tu ≈ 1 percent), a grid-generated turbulence case (Tu ≈ 7.5. percent) and two levels of large-scale turbulence generated with a mock combustor (Tu ≈ 12 and 8 percent). Exit total pressure surveys were taken at two locations to quantify total pressure losses. The suction surface boundary layer was also traversed to determine losses due to boundary layer growth. Losses occurred in the core of the flow for the elevated turbulence cases. The elevated free-stream turbulence was found to have a significant effect on wake growth. Generally, the wakes subjected to elevated free-stream turbulence were broader and had smaller peak velocity deficits. Reynolds stress profiles exhibited asymmetry in peak amplitudes about the wake centerline, which are attributable to differences in the evolution of the boundary layers on the pressure and suction surfaces of the vanes. The overall level of turbulence and dissipation inside the wakes and in the free stream was determined to document the rotor inlet boundary conditions. This is useful information for assessing rotor heat transfer and aerodynamics. Eddy diffusivities and mixing lengths were estimated using X-wire measurements of turbulent shear stress. The free-stream turbulence was found to strongly affect eddy diffusivities, and thus wake mixing. At the last measuring position, the average eddy diffusivity in the wake of the high-turbulence close combustor configuration (Tu ≈ 12) was three times that of the low turbulence wake.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Influence of Large-Scale, High-Intensity Turbulence on Vane Aerodynamic Losses, Wake Growth, and the Exit Turbulence Parameters
typeJournal Paper
journal volume119
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2841100
journal fristpage182
journal lastpage192
identifier eissn1528-8900
keywordsTurbulence
keywordsWakes
keywordsBoundary layers
keywordsEddies (Fluid dynamics)
keywordsPressure
keywordsSuction
keywordsRotors
keywordsCombustion chambers
keywordsStress
keywordsMeasurement
keywordsCascades (Fluid dynamics)
keywordsEnergy dissipation
keywordsShear (Mechanics)
keywordsChords (Trusses)
keywordsBoundary-value problems
keywordsReynolds number
keywordsWire
keywordsFlow (Dynamics)
keywordsMach number
keywordsAerodynamics AND Heat transfer
treeJournal of Turbomachinery:;1997:;volume( 119 ):;issue: 002
contenttypeFulltext


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