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    Heat Transfer Committee Best 1994 Paper Award: Experimental and Theoretical Investigations of Heat Transfer in Closed Gas-Filled Rotating Annuli II

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 001::page 11
    Author:
    D. Bohn
    ,
    R. Emunds
    ,
    V. Gorzelitz
    ,
    U. Krüger
    DOI: 10.1115/1.2836590
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Increasing the thermal efficiency by higher turbine inlet temperatures is one of the most important aims in the area of gas turbine development. Because of the high temperatures, the turbine vanes and blades have to be cooled, and also knowledge of the mechanically and thermally stressed parts in the hottest zones of the rotor is of great interest. The prediction of the temperature distribution in a gas turbine rotor containing closed, gas-filled cavities, for example, in between two disks, has to account for the heat transfer conditions encountered in these cavities. In an entirely closed annulus, forced convection is not present, but a strong natural convection flow exists, induced by a nonuniform density distribution in the centrifugal force field. In Bohn et al. (1994), experimental and numerical investigations on rotating cavities with pure centripetal heat flux had been carried out. The present paper deals with investigations on a pure axially directed heat flux. An experimental setup was designed to realize a wide range of Ra numbers (2·108 < Ra < 5·1010 ) usually encountered in cavities of gas turbine rotors. Parallel to the experiments, numerical calculations have been conducted. The numerical results are compared with the experimental data. The numerical scheme is also used to account for the influence of Re on heat transfer without changing Ra. This influence could not be pointed out by experiments, because a variation of the Re–Ra characteristic of the employed annuli was not possible. It was found that the numerical and experimental data are in quite good agreement, with exception of high Ra, where the numerical scheme predicts higher heat transfer than the experiments show. One reason may be that in the experiments the inner and outer cylindrical walls were not really adiabatic, an assumption used in the numerical procedure. Moreover, the assumption of a two-dimensional flow pattern may become invalid for high Ra. The influence of three-dimensional effects was studied with the three-dimensional version of the numerical code. In contrast to the radial directed heat transfer, it was found that Nu is much smaller and depends strongly on Re, whereas the radial heat transfer is only weakly influenced by Re.
    keyword(s): Heat transfer , Annulus , Cavities , Gas turbines , Rotors , Turbines , Flow (Dynamics) , Heat flux , High temperature , Density , Temperature distribution , Blades , Temperature , Centrifugal force , Forced convection , Disks AND Natural convection ,
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      Heat Transfer Committee Best 1994 Paper Award: Experimental and Theoretical Investigations of Heat Transfer in Closed Gas-Filled Rotating Annuli II

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    http://yetl.yabesh.ir/yetl1/handle/yetl/117888
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    • Journal of Turbomachinery

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    contributor authorD. Bohn
    contributor authorR. Emunds
    contributor authorV. Gorzelitz
    contributor authorU. Krüger
    date accessioned2017-05-08T23:52:01Z
    date available2017-05-08T23:52:01Z
    date copyrightJanuary, 1996
    date issued1996
    identifier issn0889-504X
    identifier otherJOTUEI-28648#11_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117888
    description abstractIncreasing the thermal efficiency by higher turbine inlet temperatures is one of the most important aims in the area of gas turbine development. Because of the high temperatures, the turbine vanes and blades have to be cooled, and also knowledge of the mechanically and thermally stressed parts in the hottest zones of the rotor is of great interest. The prediction of the temperature distribution in a gas turbine rotor containing closed, gas-filled cavities, for example, in between two disks, has to account for the heat transfer conditions encountered in these cavities. In an entirely closed annulus, forced convection is not present, but a strong natural convection flow exists, induced by a nonuniform density distribution in the centrifugal force field. In Bohn et al. (1994), experimental and numerical investigations on rotating cavities with pure centripetal heat flux had been carried out. The present paper deals with investigations on a pure axially directed heat flux. An experimental setup was designed to realize a wide range of Ra numbers (2·108 < Ra < 5·1010 ) usually encountered in cavities of gas turbine rotors. Parallel to the experiments, numerical calculations have been conducted. The numerical results are compared with the experimental data. The numerical scheme is also used to account for the influence of Re on heat transfer without changing Ra. This influence could not be pointed out by experiments, because a variation of the Re–Ra characteristic of the employed annuli was not possible. It was found that the numerical and experimental data are in quite good agreement, with exception of high Ra, where the numerical scheme predicts higher heat transfer than the experiments show. One reason may be that in the experiments the inner and outer cylindrical walls were not really adiabatic, an assumption used in the numerical procedure. Moreover, the assumption of a two-dimensional flow pattern may become invalid for high Ra. The influence of three-dimensional effects was studied with the three-dimensional version of the numerical code. In contrast to the radial directed heat transfer, it was found that Nu is much smaller and depends strongly on Re, whereas the radial heat transfer is only weakly influenced by Re.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer Committee Best 1994 Paper Award: Experimental and Theoretical Investigations of Heat Transfer in Closed Gas-Filled Rotating Annuli II
    typeJournal Paper
    journal volume118
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2836590
    journal fristpage11
    journal lastpage19
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsAnnulus
    keywordsCavities
    keywordsGas turbines
    keywordsRotors
    keywordsTurbines
    keywordsFlow (Dynamics)
    keywordsHeat flux
    keywordsHigh temperature
    keywordsDensity
    keywordsTemperature distribution
    keywordsBlades
    keywordsTemperature
    keywordsCentrifugal force
    keywordsForced convection
    keywordsDisks AND Natural convection
    treeJournal of Turbomachinery:;1996:;volume( 118 ):;issue: 001
    contenttypeFulltext
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