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    Capturing Mistuning Within Shrouded Integrally Bladed Disks With the Generalized Model of Mistuning

    Source: Journal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:004::page 89
    Author:
    Krizak, Troy
    ,
    D'Souza, Kiran
    DOI: 10.1115/1.4069731
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. Bladed disks and blisks are designed to be cyclic structures that ideally have identical sectors. There will, however, always be mistuning, which is blade-to-blade differences that break the cyclic symmetry of the system and can result in an increase in vibrational amplitudes. Many different methods for producing reduced order models (ROMs) have been developed, with each generally designed to accurately capture a particular form of mistuning that is present. For high-dimensional finite element (FE) models, ROMs are needed to perform many structural dynamic calculations quickly. These ROMs are also required to perform any statistical analysis to characterize random mistuning. Recently, a generalized model of mistuning (GMM) method was developed that enables efficient construction of ROMs that can readily capture multiple forms of mistuning in bladed disks simultaneously. GMM has been demonstrated to be an effective way to model mistuning separately in the blade and disk, where the mistuning can be any combination of damping, small or large stiffness, or geometric mistuning. This work extends GMM to capture systems that contain shrouds and dual flow path (DFP) blisks with multiple sources of mistuning. GMM uses only single-sector models and calculations in the construction of the ROM, allowing realistic industrial models to be analyzed. For each of the systems studied, GMM is validated using a full-stage finite element model.
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      Capturing Mistuning Within Shrouded Integrally Bladed Disks With the Generalized Model of Mistuning

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4316626
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    contributor authorKrizak, Troy
    contributor authorD'Souza, Kiran
    date accessioned2026-08-23T08:29:25Z
    date available2026-08-23T08:29:25Z
    date copyright2026/04/01
    date issued2026
    identifier issn0742-4795
    identifier othergtp-25-1458.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4316626
    description abstractAbstract. Bladed disks and blisks are designed to be cyclic structures that ideally have identical sectors. There will, however, always be mistuning, which is blade-to-blade differences that break the cyclic symmetry of the system and can result in an increase in vibrational amplitudes. Many different methods for producing reduced order models (ROMs) have been developed, with each generally designed to accurately capture a particular form of mistuning that is present. For high-dimensional finite element (FE) models, ROMs are needed to perform many structural dynamic calculations quickly. These ROMs are also required to perform any statistical analysis to characterize random mistuning. Recently, a generalized model of mistuning (GMM) method was developed that enables efficient construction of ROMs that can readily capture multiple forms of mistuning in bladed disks simultaneously. GMM has been demonstrated to be an effective way to model mistuning separately in the blade and disk, where the mistuning can be any combination of damping, small or large stiffness, or geometric mistuning. This work extends GMM to capture systems that contain shrouds and dual flow path (DFP) blisks with multiple sources of mistuning. GMM uses only single-sector models and calculations in the construction of the ROM, allowing realistic industrial models to be analyzed. For each of the systems studied, GMM is validated using a full-stage finite element model.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCapturing Mistuning Within Shrouded Integrally Bladed Disks With the Generalized Model of Mistuning
    typeJournal Paper
    journal volume148
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4069731
    journal fristpage89
    journal lastpage99
    page11
    treeJournal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:004
    contenttypeFulltext
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