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    Effect of Blade Tip Geometry on Tip Flow and Heat Transfer for a Blade in a Low-Speed Cascade

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 001::page 130
    Author:
    Vikrant Saxena
    ,
    Hasan Nasir
    ,
    Srinath V. Ekkad
    DOI: 10.1115/1.1643385
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A comprehensive investigation of the effect of various tip sealing geometries is presented on the blade tip leakage flow and associated heat transfer of a scaled up HPT turbine blade in a low-speed wind tunnel facility. The linear cascade is made of four blades with the two corner blades acting as guides. The tip section of a HPT first stage rotor blade is used to fabricate the two-dimensional blade. The wind tunnel accommodates an 116 deg turn for the blade cascade. The mainstream Reynolds number based on the axial chord length at cascade exit is 4.83×105. The upstream wake effect is simulated with a spoked wheel wake generator placed upstream of the cascade. A turbulence grid placed even farther upstream generates the required freestream turbulence of 4.8%. The center blade has a tip clearance gap of 1.5625% with respect to the blade span. Static pressure measurements are obtained on the blade surface and the shroud. The effect of crosswise trip strips to reduce leakage flow and associated heat transfer is investigated with strips placed along the leakage flow direction, against the leakage flow and along the chord. Cylindrical pin fins and pitch variation of strips over the tip surface are also investigated. Detailed heat transfer measurements are obtained using a steady-state HSI-based liquid crystal technique. The effect of periodic unsteady wake effect is also investigated by varying the wake Strouhal number from 0. to 0.2, and to 0.4. Results show that the trip strips placed against the leakage flow produce the lowest heat transfer on the tips compared to all the other cases with a reduction between 10–15% compared to the plain tip. Results also show that the pitch of the strips has a small effect on the overall reduction. Cylindrical pins fins and strips along the leakage flow direction do not decrease the heat transfer coefficients and in some cases enhance the heat transfer coefficients by as much as 20%.
    keyword(s): Flow (Dynamics) , Heat transfer , Cascades (Fluid dynamics) , Wakes , Geometry , Strips , Leakage flows , Heat transfer coefficients , Blades , Turbulence , Fins , Liquid crystals , Measurement , Pressure , Sealing (Process) AND Clearances (Engineering) ,
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      Effect of Blade Tip Geometry on Tip Flow and Heat Transfer for a Blade in a Low-Speed Cascade

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/131010
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    • Journal of Turbomachinery

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    contributor authorVikrant Saxena
    contributor authorHasan Nasir
    contributor authorSrinath V. Ekkad
    date accessioned2017-05-09T00:14:43Z
    date available2017-05-09T00:14:43Z
    date copyrightJanuary, 2004
    date issued2004
    identifier issn0889-504X
    identifier otherJOTUEI-28708#130_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131010
    description abstractA comprehensive investigation of the effect of various tip sealing geometries is presented on the blade tip leakage flow and associated heat transfer of a scaled up HPT turbine blade in a low-speed wind tunnel facility. The linear cascade is made of four blades with the two corner blades acting as guides. The tip section of a HPT first stage rotor blade is used to fabricate the two-dimensional blade. The wind tunnel accommodates an 116 deg turn for the blade cascade. The mainstream Reynolds number based on the axial chord length at cascade exit is 4.83×105. The upstream wake effect is simulated with a spoked wheel wake generator placed upstream of the cascade. A turbulence grid placed even farther upstream generates the required freestream turbulence of 4.8%. The center blade has a tip clearance gap of 1.5625% with respect to the blade span. Static pressure measurements are obtained on the blade surface and the shroud. The effect of crosswise trip strips to reduce leakage flow and associated heat transfer is investigated with strips placed along the leakage flow direction, against the leakage flow and along the chord. Cylindrical pin fins and pitch variation of strips over the tip surface are also investigated. Detailed heat transfer measurements are obtained using a steady-state HSI-based liquid crystal technique. The effect of periodic unsteady wake effect is also investigated by varying the wake Strouhal number from 0. to 0.2, and to 0.4. Results show that the trip strips placed against the leakage flow produce the lowest heat transfer on the tips compared to all the other cases with a reduction between 10–15% compared to the plain tip. Results also show that the pitch of the strips has a small effect on the overall reduction. Cylindrical pins fins and strips along the leakage flow direction do not decrease the heat transfer coefficients and in some cases enhance the heat transfer coefficients by as much as 20%.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Blade Tip Geometry on Tip Flow and Heat Transfer for a Blade in a Low-Speed Cascade
    typeJournal Paper
    journal volume126
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1643385
    journal fristpage130
    journal lastpage138
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsHeat transfer
    keywordsCascades (Fluid dynamics)
    keywordsWakes
    keywordsGeometry
    keywordsStrips
    keywordsLeakage flows
    keywordsHeat transfer coefficients
    keywordsBlades
    keywordsTurbulence
    keywordsFins
    keywordsLiquid crystals
    keywordsMeasurement
    keywordsPressure
    keywordsSealing (Process) AND Clearances (Engineering)
    treeJournal of Turbomachinery:;2004:;volume( 126 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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