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    Extended Windage Loss Models for Gas Bearing Supported Spindles Operated in Dense Gases

    Source: Journal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 006::page 061010-1
    Author:
    Rosset, Kévin
    ,
    Schiffmann, Jürg
    DOI: 10.1115/1.4047124
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Generic models are proposed to evaluate the skin friction coefficient acting on enclosed rotating disks and cylinders under various flow regimes. In particular, a model taking into account the inner radius of the disk is developed. The models are compared with experimental data obtained from coast-down tests of a high-speed spindle supported on gas lubricated bearings, operated in air and in halocarbon R245fa at various pressures. The windage losses are first computed considering state-of-the-art laminar flow loss models in the gas bearings and an experimentally validated laminar-turbulent flow loss model in the air gap. This reference approach predicts the air data with a good accuracy (deviation less than 5%) but underestimates the organic fluid data by up to 36%. This deviation is considerably reduced (max 6.8%) when applying the proposed multiflow regime loss model for enclosed rotating disks to the thrust bearing. Finally, the proposed laminar-turbulent flow loss model for enclosed rotating cylinders is simultaneously applied to the journal bearings and the air gap. A peak deviation of 6.5% is maintained among all test cases when setting the critical Taylor number to an artificial value (67) instead of the theoretical value (41.1) characterizing the onset of growth of Taylor vortices. Taking into account the uncertainties on the bearing clearances, as well as on the operating pressure and temperature, a ±10% agreement with the experimental data is obtained.
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      Extended Windage Loss Models for Gas Bearing Supported Spindles Operated in Dense Gases

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    contributor authorRosset, Kévin
    contributor authorSchiffmann, Jürg
    date accessioned2022-02-04T21:59:33Z
    date available2022-02-04T21:59:33Z
    date copyright5/29/2020 12:00:00 AM
    date issued2020
    identifier issn0742-4795
    identifier othergtp_142_06_061010.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4274664
    description abstractGeneric models are proposed to evaluate the skin friction coefficient acting on enclosed rotating disks and cylinders under various flow regimes. In particular, a model taking into account the inner radius of the disk is developed. The models are compared with experimental data obtained from coast-down tests of a high-speed spindle supported on gas lubricated bearings, operated in air and in halocarbon R245fa at various pressures. The windage losses are first computed considering state-of-the-art laminar flow loss models in the gas bearings and an experimentally validated laminar-turbulent flow loss model in the air gap. This reference approach predicts the air data with a good accuracy (deviation less than 5%) but underestimates the organic fluid data by up to 36%. This deviation is considerably reduced (max 6.8%) when applying the proposed multiflow regime loss model for enclosed rotating disks to the thrust bearing. Finally, the proposed laminar-turbulent flow loss model for enclosed rotating cylinders is simultaneously applied to the journal bearings and the air gap. A peak deviation of 6.5% is maintained among all test cases when setting the critical Taylor number to an artificial value (67) instead of the theoretical value (41.1) characterizing the onset of growth of Taylor vortices. Taking into account the uncertainties on the bearing clearances, as well as on the operating pressure and temperature, a ±10% agreement with the experimental data is obtained.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleExtended Windage Loss Models for Gas Bearing Supported Spindles Operated in Dense Gases
    typeJournal Paper
    journal volume142
    journal issue6
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4047124
    journal fristpage061010-1
    journal lastpage061010-15
    page15
    treeJournal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 006
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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