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    Geometric Mistuning Identification of Integrally Bladed Rotors Using Modified Modal Domain Analysis

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 012::page 122504
    Author:
    Bhartiya, Yasharth
    ,
    Sinha, Alok
    DOI: 10.1115/1.4027762
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Modified modal domain analysis (MMDA) is a novel method for the development of a reduced order model of a bladed rotor with geometric mistuning. This method utilizes proper orthogonal decomposition (POD) of coordinate measurement machine (CMM) data on blades' geometries, and sector analyses using ansys and solid modeling. In a recent paper, MMDA has been extended to use second order Taylor series approximations of perturbations in mass and stiffness matrices (خ´M and خ´K) instead of exact خ´M and خ´K. Taylor series expansions of deviations in mass and stiffness matrices due to geometric mistuning give a direct approach for generating the reduced order model from the components of POD features of spatial variations in blades' geometries. Reversing the process, algorithms for mistuning identification based on MMDA are presented in this paper to calculate the geometric mistuning parameters. Two types of algorithm, one based on modal analyses and the other on the forced responses, are presented. The validity of these methods are then verified through a mistuned academic rotor.
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      Geometric Mistuning Identification of Integrally Bladed Rotors Using Modified Modal Domain Analysis

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    https://yetl.yabesh.ir/yetl1/handle/yetl/154869
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorBhartiya, Yasharth
    contributor authorSinha, Alok
    date accessioned2017-05-09T01:08:11Z
    date available2017-05-09T01:08:11Z
    date issued2014
    identifier issn1528-8919
    identifier othergtp_136_12_122504.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154869
    description abstractModified modal domain analysis (MMDA) is a novel method for the development of a reduced order model of a bladed rotor with geometric mistuning. This method utilizes proper orthogonal decomposition (POD) of coordinate measurement machine (CMM) data on blades' geometries, and sector analyses using ansys and solid modeling. In a recent paper, MMDA has been extended to use second order Taylor series approximations of perturbations in mass and stiffness matrices (خ´M and خ´K) instead of exact خ´M and خ´K. Taylor series expansions of deviations in mass and stiffness matrices due to geometric mistuning give a direct approach for generating the reduced order model from the components of POD features of spatial variations in blades' geometries. Reversing the process, algorithms for mistuning identification based on MMDA are presented in this paper to calculate the geometric mistuning parameters. Two types of algorithm, one based on modal analyses and the other on the forced responses, are presented. The validity of these methods are then verified through a mistuned academic rotor.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleGeometric Mistuning Identification of Integrally Bladed Rotors Using Modified Modal Domain Analysis
    typeJournal Paper
    journal volume136
    journal issue12
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4027762
    journal fristpage122504
    journal lastpage122504
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 012
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian