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    The Influence of Large-Scale, High-Intensity Turbulence on Vane Aerodynamic Losses, Wake Growth, and the Exit Turbulence Parameters

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 002::page 182
    Author:
    F. E. Ames
    ,
    M. W. Plesniak
    DOI: 10.1115/1.2841100
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An 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.
    keyword(s): Turbulence , Wakes , Boundary layers , Eddies (Fluid dynamics) , Pressure , Suction , Rotors , Combustion chambers , Stress , Measurement , Cascades (Fluid dynamics) , Energy dissipation , Shear (Mechanics) , Chords (Trusses) , Boundary-value problems , Reynolds number , Wire , Flow (Dynamics) , Mach number , Aerodynamics AND Heat transfer ,
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      The Influence of Large-Scale, High-Intensity Turbulence on Vane Aerodynamic Losses, Wake Growth, and the Exit Turbulence Parameters

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/119624
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    • Journal of Turbomachinery

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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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