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    Detection of Damage in Space Frame Structures With L Shaped Beams and Bolted Joints Using Changes in Natural Frequencies

    Source: Journal of Vibration and Acoustics:;2013:;volume( 135 ):;issue: 005::page 51001
    Author:
    Zhu, W. D.
    ,
    He, K.
    DOI: 10.1115/1.4024393
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: It is difficult to use conventional nondestructive testing methods to detect damage, such as loosening of bolted connections, in a space frame structure due to the complexity of the structure and the nature of the possible damage. A vibrationbased method that uses changes in the natural frequencies of a structure to detect the locations and extent of damage in it has the advantage of being able to detect various types of damage in the structure, including loosening of bolted connections. Since the vibrationbased method is modelbased, applying it to a space frame structure with Lshaped beams and bolted joints will face challenges ranging from the development of an accurate dynamic model of the structure to that of a robust damage detection algorithm for a severely underdetermined, nonlinear leastsquare problem under the effects of relatively large modeling error and measurement noise. With the development of modeling techniques for fillets in thinwalled beams (He and Zhu, 2009, “Modeling of Fillets in ThinWalled Beams Using Shell/Plate and Beam Finite Elements,â€‌ ASME J. Vib. Acoust., 131 (5), p. 051002) and bolted joints (He and Zhu, 2011, “Finite Element Modeling of Structures With Lshaped Beams and Bolted Joints,â€‌ ASME J. Vib. Acoust., 131(1), p. 011010) by the authors, accurate physicsbased models of space frame structures can be developed with a reasonable model size. A new damage detection algorithm that uses a trustregion search strategy combined with a logistic function transformation is developed to improve the robustness of the vibrationbased damage detection method. The new algorithm can ensure global convergence of the iterations and minimize the effects of modeling error and measurement noise. The damage detection method developed is experimentally validated on an aluminum threebay space frame structure with Lshaped beams and bolted joints. Three types of introduced damage, including joint damage, member damage, and boundary damage, were successfully detected. In the numerical simulation where there are no modeling error and measurement noise, the almost exact locations and extent of damage can be detected.
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      Detection of Damage in Space Frame Structures With L Shaped Beams and Bolted Joints Using Changes in Natural Frequencies

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    http://yetl.yabesh.ir/yetl1/handle/yetl/153628
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    contributor authorZhu, W. D.
    contributor authorHe, K.
    date accessioned2017-05-09T01:04:17Z
    date available2017-05-09T01:04:17Z
    date issued2013
    identifier issn1048-9002
    identifier othervib_135_5_051001.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153628
    description abstractIt is difficult to use conventional nondestructive testing methods to detect damage, such as loosening of bolted connections, in a space frame structure due to the complexity of the structure and the nature of the possible damage. A vibrationbased method that uses changes in the natural frequencies of a structure to detect the locations and extent of damage in it has the advantage of being able to detect various types of damage in the structure, including loosening of bolted connections. Since the vibrationbased method is modelbased, applying it to a space frame structure with Lshaped beams and bolted joints will face challenges ranging from the development of an accurate dynamic model of the structure to that of a robust damage detection algorithm for a severely underdetermined, nonlinear leastsquare problem under the effects of relatively large modeling error and measurement noise. With the development of modeling techniques for fillets in thinwalled beams (He and Zhu, 2009, “Modeling of Fillets in ThinWalled Beams Using Shell/Plate and Beam Finite Elements,â€‌ ASME J. Vib. Acoust., 131 (5), p. 051002) and bolted joints (He and Zhu, 2011, “Finite Element Modeling of Structures With Lshaped Beams and Bolted Joints,â€‌ ASME J. Vib. Acoust., 131(1), p. 011010) by the authors, accurate physicsbased models of space frame structures can be developed with a reasonable model size. A new damage detection algorithm that uses a trustregion search strategy combined with a logistic function transformation is developed to improve the robustness of the vibrationbased damage detection method. The new algorithm can ensure global convergence of the iterations and minimize the effects of modeling error and measurement noise. The damage detection method developed is experimentally validated on an aluminum threebay space frame structure with Lshaped beams and bolted joints. Three types of introduced damage, including joint damage, member damage, and boundary damage, were successfully detected. In the numerical simulation where there are no modeling error and measurement noise, the almost exact locations and extent of damage can be detected.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDetection of Damage in Space Frame Structures With L Shaped Beams and Bolted Joints Using Changes in Natural Frequencies
    typeJournal Paper
    journal volume135
    journal issue5
    journal titleJournal of Vibration and Acoustics
    identifier doi10.1115/1.4024393
    journal fristpage51001
    journal lastpage51001
    identifier eissn1528-8927
    treeJournal of Vibration and Acoustics:;2013:;volume( 135 ):;issue: 005
    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