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    Phase-Averaged Wall Shear Stress, Wall Pressure, and Near-Wall Velocity Field Measurements in a Whirling Annular Seal

    Source: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 003::page 590
    Author:
    G. L. Morrison
    ,
    R. B. Winslow
    ,
    H. D. Thames
    DOI: 10.1115/1.2816689
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow field inside a 50 percent eccentric whirling annular seal operating at a Reynolds number of 24,000 and a Taylor number of 6600 has been measured using a three-dimensional laser-Doppler anemometer system. Flush mount pressure and wall shear stress probes have been used to measure the stresses (normal and shear) along the length of the stator. The rotor was mounted eccentrically on the shaft so that the rotor orbit was circular and rotated at the same speed as the shaft (a whirl ratio of 1.0). This paper presents mean pressure, mean wall shear stress magnitude, and mean wall shear stress direction distributions along the length of the seal. Phase-averaged wall pressure and wall shear stress are presented along with phase-averaged mean velocity and turbulence kinetic energy distributions located 0.16c from the stator wall, where c is the seal clearance. The relationships between the velocity, turbulence, wall pressure, and wall shear stress are very complex and do not follow simple bulk flow predictions.
    keyword(s): Measurement , Pressure , Stress , Shear (Mechanics) , Whirls , Stators , Rotors , Flow (Dynamics) , Turbulence , Kinetic energy , Reynolds number , Lasers , Clearances (Engineering) AND Probes ,
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      Phase-Averaged Wall Shear Stress, Wall Pressure, and Near-Wall Velocity Field Measurements in a Whirling Annular Seal

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/116910
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorG. L. Morrison
    contributor authorR. B. Winslow
    contributor authorH. D. Thames
    date accessioned2017-05-08T23:50:05Z
    date available2017-05-08T23:50:05Z
    date copyrightJuly, 1996
    date issued1996
    identifier issn1528-8919
    identifier otherJETPEZ-26756#590_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116910
    description abstractThe flow field inside a 50 percent eccentric whirling annular seal operating at a Reynolds number of 24,000 and a Taylor number of 6600 has been measured using a three-dimensional laser-Doppler anemometer system. Flush mount pressure and wall shear stress probes have been used to measure the stresses (normal and shear) along the length of the stator. The rotor was mounted eccentrically on the shaft so that the rotor orbit was circular and rotated at the same speed as the shaft (a whirl ratio of 1.0). This paper presents mean pressure, mean wall shear stress magnitude, and mean wall shear stress direction distributions along the length of the seal. Phase-averaged wall pressure and wall shear stress are presented along with phase-averaged mean velocity and turbulence kinetic energy distributions located 0.16c from the stator wall, where c is the seal clearance. The relationships between the velocity, turbulence, wall pressure, and wall shear stress are very complex and do not follow simple bulk flow predictions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePhase-Averaged Wall Shear Stress, Wall Pressure, and Near-Wall Velocity Field Measurements in a Whirling Annular Seal
    typeJournal Paper
    journal volume118
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2816689
    journal fristpage590
    journal lastpage597
    identifier eissn0742-4795
    keywordsMeasurement
    keywordsPressure
    keywordsStress
    keywordsShear (Mechanics)
    keywordsWhirls
    keywordsStators
    keywordsRotors
    keywordsFlow (Dynamics)
    keywordsTurbulence
    keywordsKinetic energy
    keywordsReynolds number
    keywordsLasers
    keywordsClearances (Engineering) AND Probes
    treeJournal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 003
    contenttypeFulltext
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