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    Effects of the Geometric Uncertainties of Bladed Disks Through the Analytical Derivatives of the Finite Element Matrices

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 006::page 61022-1
    Author:
    Bouras, Abdelhakim
    ,
    Carassale, Luigi
    DOI: 10.1115/1.4066894
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Manufacturing processes and wear are known to create imperfections in mechanical components that may result in a significant deviation of the modal properties from their predicted values. This is especially true for periodic structures such as bladed disks, where even small variations in the blade geometry can cause mistuning. The effect of parameter variations on the model is commonly assessed through sensitivity analysis within the framework of uncertainty propagation or structural optimization. Different formulations are available when dealing with the variation of a single scalar parameter. The problem becomes more complicated when the source of the variation is the whole component geometry. To deal with this case, it is necessary to define a representation able to describe the shift from the nominal geometry through a finite set of parameters and compute the derivatives of the system matrices with respect to those parameters. This paper proposes to compute analytically the derivatives of the system matrices with respect to the geometric variations. The derivatives are calculated at the finite element (FE) level and are then assembled into global derivative matrices. Using directional derivatives, the sensitivities of the system matrices are computed with standard FE numerical schemes based on the nominal geometry.
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      Effects of the Geometric Uncertainties of Bladed Disks Through the Analytical Derivatives of the Finite Element Matrices

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4305741
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    contributor authorBouras, Abdelhakim
    contributor authorCarassale, Luigi
    date accessioned2025-04-21T10:13:26Z
    date available2025-04-21T10:13:26Z
    date copyright12/20/2024 12:00:00 AM
    date issued2024
    identifier issn0742-4795
    identifier othergtp_147_06_061022.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4305741
    description abstractManufacturing processes and wear are known to create imperfections in mechanical components that may result in a significant deviation of the modal properties from their predicted values. This is especially true for periodic structures such as bladed disks, where even small variations in the blade geometry can cause mistuning. The effect of parameter variations on the model is commonly assessed through sensitivity analysis within the framework of uncertainty propagation or structural optimization. Different formulations are available when dealing with the variation of a single scalar parameter. The problem becomes more complicated when the source of the variation is the whole component geometry. To deal with this case, it is necessary to define a representation able to describe the shift from the nominal geometry through a finite set of parameters and compute the derivatives of the system matrices with respect to those parameters. This paper proposes to compute analytically the derivatives of the system matrices with respect to the geometric variations. The derivatives are calculated at the finite element (FE) level and are then assembled into global derivative matrices. Using directional derivatives, the sensitivities of the system matrices are computed with standard FE numerical schemes based on the nominal geometry.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffects of the Geometric Uncertainties of Bladed Disks Through the Analytical Derivatives of the Finite Element Matrices
    typeJournal Paper
    journal volume147
    journal issue6
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4066894
    journal fristpage61022-1
    journal lastpage61022-8
    page8
    treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 006
    contenttypeFulltext
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