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    A Study of the Modal Truncation Error in the Component Mode Analysis of a Dual-Rotor System

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 003::page 525
    Author:
    D. F. Li
    ,
    E. J. Gunter
    DOI: 10.1115/1.3227311
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the component mode synthesis method, the equation of motion in the generalized coordinates is built upon the undamped eigenvalue data of the component structures. Error is inevitable when truncated modes are used. In this paper, two model truncation schemes were evaluated with regard to the critical speed, stability, and unbalance response of a two-spool gas turbine engine. The numbers of modes required to yield acceptable accuracy in these cases were determined. Guidelines for modal truncation were derived from these results.
    keyword(s): Rotors , Errors , Eigenvalues , Stability , Equations of motion AND Gas turbines ,
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      A Study of the Modal Truncation Error in the Component Mode Analysis of a Dual-Rotor System

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    http://yetl.yabesh.ir/yetl1/handle/yetl/95752
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorD. F. Li
    contributor authorE. J. Gunter
    date accessioned2017-05-08T23:13:10Z
    date available2017-05-08T23:13:10Z
    date copyrightJuly, 1982
    date issued1982
    identifier issn1528-8919
    identifier otherJETPEZ-26776#525_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/95752
    description abstractIn the component mode synthesis method, the equation of motion in the generalized coordinates is built upon the undamped eigenvalue data of the component structures. Error is inevitable when truncated modes are used. In this paper, two model truncation schemes were evaluated with regard to the critical speed, stability, and unbalance response of a two-spool gas turbine engine. The numbers of modes required to yield acceptable accuracy in these cases were determined. Guidelines for modal truncation were derived from these results.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Study of the Modal Truncation Error in the Component Mode Analysis of a Dual-Rotor System
    typeJournal Paper
    journal volume104
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227311
    journal fristpage525
    journal lastpage532
    identifier eissn0742-4795
    keywordsRotors
    keywordsErrors
    keywordsEigenvalues
    keywordsStability
    keywordsEquations of motion AND Gas turbines
    treeJournal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 003
    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
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