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    Parametric Reduced Order Models for Bladed Disks With Mistuning and Varying Operational Speed

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 005::page 51018
    Author:
    Kurstak, Eric
    ,
    Wilber, Ryan
    ,
    D'Souza, Kiran
    DOI: 10.1115/1.4041204
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: A considerable amount of research has been conducted to develop reduced order models (ROMs) of bladed disks that can be constructed using single sector calculations when there is mistuning present. A variety of methods have been developed to efficiently handle different types of mistuning ranging from small frequency mistuning, which can be modeled using a variety of methods including component mode mistuning (CMM), to large geometric mistuning, which can be modeled using multiple techniques including pristine rogue interface modal expansion (PRIME). Research has also been conducted on developing ROMs that can accommodate the variation of specific parameters in the reduced space; these models are referred to as parametric reduced order models (PROMs). This work introduces a PROM for bladed disks that allows for the variation of rotational speed in the reduced space. These PROMs are created by extracting information from sector models at three rotational speeds, and then the appropriate ROM is efficiently constructed in the reduced space at any other desired speed. This work integrates these new PROMs for bladed disks with two existing mistuning methods, CMM and PRIME, to illustrate how the method can be readily applied for a variety of mistuning methods. Frequencies and forced response calculations using these new PROMs are compared to the full order finite element calculations to demonstrate the effectiveness of the method.
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      Parametric Reduced Order Models for Bladed Disks With Mistuning and Varying Operational Speed

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    contributor authorKurstak, Eric
    contributor authorWilber, Ryan
    contributor authorD'Souza, Kiran
    date accessioned2019-09-18T09:04:30Z
    date available2019-09-18T09:04:30Z
    date copyright3/8/2019 12:00:00 AM
    date issued2019
    identifier issn0742-4795
    identifier othergtp_141_05_051018.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4258553
    description abstractA considerable amount of research has been conducted to develop reduced order models (ROMs) of bladed disks that can be constructed using single sector calculations when there is mistuning present. A variety of methods have been developed to efficiently handle different types of mistuning ranging from small frequency mistuning, which can be modeled using a variety of methods including component mode mistuning (CMM), to large geometric mistuning, which can be modeled using multiple techniques including pristine rogue interface modal expansion (PRIME). Research has also been conducted on developing ROMs that can accommodate the variation of specific parameters in the reduced space; these models are referred to as parametric reduced order models (PROMs). This work introduces a PROM for bladed disks that allows for the variation of rotational speed in the reduced space. These PROMs are created by extracting information from sector models at three rotational speeds, and then the appropriate ROM is efficiently constructed in the reduced space at any other desired speed. This work integrates these new PROMs for bladed disks with two existing mistuning methods, CMM and PRIME, to illustrate how the method can be readily applied for a variety of mistuning methods. Frequencies and forced response calculations using these new PROMs are compared to the full order finite element calculations to demonstrate the effectiveness of the method.
    publisherAmerican Society of Mechanical Engineers (ASME)
    titleParametric Reduced Order Models for Bladed Disks With Mistuning and Varying Operational Speed
    typeJournal Paper
    journal volume141
    journal issue5
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4041204
    journal fristpage51018
    journal lastpage051018-9
    treeJournal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 005
    contenttypeFulltext
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