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    The Effect of Side Wall Mass Extraction on Pressure Loss and Heat Transfer of a Ribbed Rectangular Two-Pass Internal Cooling Channel

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 002::page 21002
    Author:
    Marco Schüler
    ,
    Frank Zehnder
    ,
    Bernhard Weigand
    ,
    Jens von Wolfersdorf
    ,
    Sven Olaf Neumann
    DOI: 10.1115/1.4000552
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Gas turbine blades are often cooled by using combined internal and external cooling methods where for internal cooling purposes, usually, serpentine passages are applied. In order to optimize the design of these serpentine passages it is inevitable to know the influence of mass extraction due to film cooling holes, dust holes, or due to side walls for feeding successive cooling channels as for the trailing edge on the internal cooling performance. Therefore, the objective of the present study was to analyze the influence of side wall mass extraction on pressure loss and heat transfer distribution in a two-pass internal cooling channel representing a cooling scheme with flow towards the trailing edge. The investigated rectangular two-pass channel consisted of an inlet and outlet duct with a height-to-width ratio of H/W=2 connected by a 180 deg sharp bend. The tip-to-web distance was kept constant at Wel/W=1. The mass extraction was realized using several circular holes in the outlet pass side wall. Two geometric configurations were investigated: A configuration with mass extraction solely in the outlet pass and a configuration with mass extraction in the bend region and outlet pass. The extracted mass flow rate was 0%, 10%, and 20% of the inlet channel mass flow. Spatially resolved heat transfer distributions were obtained using the transient thermochromic liquid crystal technique. Pressure losses were determined in separate experiments by local static pressure measurements. Furthermore, a computational study was performed solving the Reynolds-averaged Navier–Stokes equations using the commercial finite-volume solver FLUENT . The numerical grids were generated using the hybrid grid generator CENTAUR . Three different turbulence models were considered: the realizable k-ε model with two-layer wall treatment, the k-ω-SST model, and the v2-f model. The experimental data of the investigation of side wall ejection showed that the heat transfer in the bend region slightly increased when the ejection were in operation, while the heat transfer in the section of the outlet channel with side wall ejection was nearly not affected. After this section, a decrease in heat transfer was observed, which can be attributed to the decreased mainstream mass flow rate.
    keyword(s): Heat transfer , Cooling , Channels (Hydraulic engineering) , Pressure , Flow (Dynamics) , Turbulence AND Temperature ,
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      The Effect of Side Wall Mass Extraction on Pressure Loss and Heat Transfer of a Ribbed Rectangular Two-Pass Internal Cooling Channel

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/147819
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    • Journal of Turbomachinery

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    contributor authorMarco Schüler
    contributor authorFrank Zehnder
    contributor authorBernhard Weigand
    contributor authorJens von Wolfersdorf
    contributor authorSven Olaf Neumann
    date accessioned2017-05-09T00:47:26Z
    date available2017-05-09T00:47:26Z
    date copyrightApril, 2011
    date issued2011
    identifier issn0889-504X
    identifier otherJOTUEI-28770#021002_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/147819
    description abstractGas turbine blades are often cooled by using combined internal and external cooling methods where for internal cooling purposes, usually, serpentine passages are applied. In order to optimize the design of these serpentine passages it is inevitable to know the influence of mass extraction due to film cooling holes, dust holes, or due to side walls for feeding successive cooling channels as for the trailing edge on the internal cooling performance. Therefore, the objective of the present study was to analyze the influence of side wall mass extraction on pressure loss and heat transfer distribution in a two-pass internal cooling channel representing a cooling scheme with flow towards the trailing edge. The investigated rectangular two-pass channel consisted of an inlet and outlet duct with a height-to-width ratio of H/W=2 connected by a 180 deg sharp bend. The tip-to-web distance was kept constant at Wel/W=1. The mass extraction was realized using several circular holes in the outlet pass side wall. Two geometric configurations were investigated: A configuration with mass extraction solely in the outlet pass and a configuration with mass extraction in the bend region and outlet pass. The extracted mass flow rate was 0%, 10%, and 20% of the inlet channel mass flow. Spatially resolved heat transfer distributions were obtained using the transient thermochromic liquid crystal technique. Pressure losses were determined in separate experiments by local static pressure measurements. Furthermore, a computational study was performed solving the Reynolds-averaged Navier–Stokes equations using the commercial finite-volume solver FLUENT . The numerical grids were generated using the hybrid grid generator CENTAUR . Three different turbulence models were considered: the realizable k-ε model with two-layer wall treatment, the k-ω-SST model, and the v2-f model. The experimental data of the investigation of side wall ejection showed that the heat transfer in the bend region slightly increased when the ejection were in operation, while the heat transfer in the section of the outlet channel with side wall ejection was nearly not affected. After this section, a decrease in heat transfer was observed, which can be attributed to the decreased mainstream mass flow rate.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Effect of Side Wall Mass Extraction on Pressure Loss and Heat Transfer of a Ribbed Rectangular Two-Pass Internal Cooling Channel
    typeJournal Paper
    journal volume133
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4000552
    journal fristpage21002
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsCooling
    keywordsChannels (Hydraulic engineering)
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsTurbulence AND Temperature
    treeJournal of Turbomachinery:;2011:;volume( 133 ):;issue: 002
    contenttypeFulltext
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