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    High Throughflow StreamVane Swirl Distortion Generators: Design and Analysis

    Source: Journal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 004::page 41014-1
    Author:
    Hayden, Andrew P.
    ,
    Gillespie, John
    ,
    Hefner, Cole
    ,
    Untaroiu, Alexandrina
    ,
    Lowe, K. Todd
    DOI: 10.1115/1.4063709
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In recent years, the StreamVane technology has developed into a mature and streamlined process that can reproduce swirl distortion for ground-test evaluation of fan and compressor performance and durability. A StreamVane device consists of complex turning vanes that accurately output a distorted secondary velocity field at a defined distance downstream. To further advance the applications and conditions in which these devices operate, a research effort was developed and completed to investigate methods to increase critical Mach numbers. The effort was split into three separate stages: (1) Perform high fidelity computational fluid dynamics (CFD) to identify peak Mach number locations within twin and quad swirl vane pack designs; (2) conduct thorough literature reviews on relevant high throughflow techniques; and (3) design and implement selected techniques to evaluate improvements using the same high-fidelity CFD methods. It was predicted that employing blade lean within high-speed vane junctions increased critical Mach numbers by 6.6%, while blade sweep resulted in a 3.5% increase. The results and conclusions from this effort are presented throughout this paper with a primary focus on comparing Mach numbers and swirl profiles between vane packs with and without high throughflow designs.
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      High Throughflow StreamVane Swirl Distortion Generators: Design and Analysis

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4295207
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    contributor authorHayden, Andrew P.
    contributor authorGillespie, John
    contributor authorHefner, Cole
    contributor authorUntaroiu, Alexandrina
    contributor authorLowe, K. Todd
    date accessioned2024-04-24T22:25:54Z
    date available2024-04-24T22:25:54Z
    date copyright12/8/2023 12:00:00 AM
    date issued2023
    identifier issn0742-4795
    identifier othergtp_146_04_041014.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4295207
    description abstractIn recent years, the StreamVane technology has developed into a mature and streamlined process that can reproduce swirl distortion for ground-test evaluation of fan and compressor performance and durability. A StreamVane device consists of complex turning vanes that accurately output a distorted secondary velocity field at a defined distance downstream. To further advance the applications and conditions in which these devices operate, a research effort was developed and completed to investigate methods to increase critical Mach numbers. The effort was split into three separate stages: (1) Perform high fidelity computational fluid dynamics (CFD) to identify peak Mach number locations within twin and quad swirl vane pack designs; (2) conduct thorough literature reviews on relevant high throughflow techniques; and (3) design and implement selected techniques to evaluate improvements using the same high-fidelity CFD methods. It was predicted that employing blade lean within high-speed vane junctions increased critical Mach numbers by 6.6%, while blade sweep resulted in a 3.5% increase. The results and conclusions from this effort are presented throughout this paper with a primary focus on comparing Mach numbers and swirl profiles between vane packs with and without high throughflow designs.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHigh Throughflow StreamVane Swirl Distortion Generators: Design and Analysis
    typeJournal Paper
    journal volume146
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4063709
    journal fristpage41014-1
    journal lastpage41014-12
    page12
    treeJournal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 004
    contenttypeFulltext
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