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    A Generalization of Effective Mass for Selecting Free–Free Target Modes

    Source: Journal of Vibration and Acoustics:;2007:;volume( 129 ):;issue: 001::page 121
    Author:
    Daniel C. Kammer
    ,
    Andrew Kostuch
    ,
    Joseph Cessna
    DOI: 10.1115/1.2424980
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: One of the most important tasks in pretest analysis and modal survey planning is the selection of target modes. The target modes are those mode shapes that are determined to be dynamically important using some definition. While there are many measures of dynamic importance, one of the measures that has been of greatest interest to structural dynamicists, is the contribution of each mode to the dynamic loads at an interface. Dynamically important modes contribute significantly to the interface loads and must be retained in any reduced analytical representation. These modes must be identified during a ground vibration test to validate the corresponding finite element model. Structural dynamicists have used interface load based effective mass measures to efficiently identify target modes for constrained structures. The advantage of these measures of dynamic importance is that they are absolute, in contrast to other measures that only indicate the importance of one mode shape relative to another. However, in many situations, especially in aerospace applications, structures must be tested in a free–free configuration. In the case of free–free elastic modes, the effective mass values are zero, making them useless measures of dynamic importance. This paper presents a new effective mass like measure of absolute dynamic importance that can be applied to free–free structures. The new method is derived based upon the free–free modal equations of motion. The approach is shown to be directly related to ranking mode shapes based on approximate balanced singular values. But, unlike the approximate balanced singular value approach, it is an absolute measure of importance. A numerical example of a general spacecraft system is presented to illustrate the application of the new technique. Dynamically important mode shapes were easily identified for modal acceleration, velocity, and displacement output. The new method provides an efficient technique for selecting target modes for a modal vibration test, or the reduction of a modal based analytical model to the dynamically important mode shapes.
    keyword(s): Electromagnetic fields , Stress , Displacement , Finite element model , Shapes , Space vehicles , Equations of motion , Enterprise information management , Vibration tests , Degrees of freedom AND Aerospace industry ,
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      A Generalization of Effective Mass for Selecting Free–Free Target Modes

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    https://yetl.yabesh.ir/yetl1/handle/yetl/137176
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    • Journal of Vibration and Acoustics

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    contributor authorDaniel C. Kammer
    contributor authorAndrew Kostuch
    contributor authorJoseph Cessna
    date accessioned2017-05-09T00:26:27Z
    date available2017-05-09T00:26:27Z
    date copyrightFebruary, 2007
    date issued2007
    identifier issn1048-9002
    identifier otherJVACEK-28884#121_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137176
    description abstractOne of the most important tasks in pretest analysis and modal survey planning is the selection of target modes. The target modes are those mode shapes that are determined to be dynamically important using some definition. While there are many measures of dynamic importance, one of the measures that has been of greatest interest to structural dynamicists, is the contribution of each mode to the dynamic loads at an interface. Dynamically important modes contribute significantly to the interface loads and must be retained in any reduced analytical representation. These modes must be identified during a ground vibration test to validate the corresponding finite element model. Structural dynamicists have used interface load based effective mass measures to efficiently identify target modes for constrained structures. The advantage of these measures of dynamic importance is that they are absolute, in contrast to other measures that only indicate the importance of one mode shape relative to another. However, in many situations, especially in aerospace applications, structures must be tested in a free–free configuration. In the case of free–free elastic modes, the effective mass values are zero, making them useless measures of dynamic importance. This paper presents a new effective mass like measure of absolute dynamic importance that can be applied to free–free structures. The new method is derived based upon the free–free modal equations of motion. The approach is shown to be directly related to ranking mode shapes based on approximate balanced singular values. But, unlike the approximate balanced singular value approach, it is an absolute measure of importance. A numerical example of a general spacecraft system is presented to illustrate the application of the new technique. Dynamically important mode shapes were easily identified for modal acceleration, velocity, and displacement output. The new method provides an efficient technique for selecting target modes for a modal vibration test, or the reduction of a modal based analytical model to the dynamically important mode shapes.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Generalization of Effective Mass for Selecting Free–Free Target Modes
    typeJournal Paper
    journal volume129
    journal issue1
    journal titleJournal of Vibration and Acoustics
    identifier doi10.1115/1.2424980
    journal fristpage121
    journal lastpage127
    identifier eissn1528-8927
    keywordsElectromagnetic fields
    keywordsStress
    keywordsDisplacement
    keywordsFinite element model
    keywordsShapes
    keywordsSpace vehicles
    keywordsEquations of motion
    keywordsEnterprise information management
    keywordsVibration tests
    keywordsDegrees of freedom AND Aerospace industry
    treeJournal of Vibration and Acoustics:;2007:;volume( 129 ):;issue: 001
    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