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    Assessments of Structural Health Monitoring for Fatigue Cracks in Metallic Structures by Using Lamb Waves Driven by Piezoelectric Transducers

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 001::page 04020091
    Author:
    Chung-De Chen
    ,
    Yu-Cheng Chiu
    ,
    Yao-Hung Huang
    ,
    Po-Hao Wang
    ,
    Rong-Der Chien
    DOI: 10.1061/(ASCE)AS.1943-5525.0001212
    Publisher: ASCE
    Abstract: In this paper, the assessments of structural health monitoring (SHM) for metallic structures are presented. Tests were conducted on three specimens for fatigue crack testing and damage index measurements. In each specimen, a transducer array of six Stanford Multiactuator-Receiver Transduction (SMART) Layers, each of which contains a piezoelectric transducer, was mounted near the fatigue crack. The Lamb wave was driven by one SMART Layer and received by another. The transducer array generated nine forward and nine backward propagating paths. The damage index defined in the first arrival window (FAW) was obtained for each path. In this work, we propose an averaging process to obtain average damage index from the transducer array. The Lamb waves with various driving frequencies were tested to conduct the performance of the damage monitoring. The results show that the plot of the average damage index versus the actual crack length reveals a narrow band, indicating a small standard deviation of the measurement data. The data of numerous crack lengths and Lamb wave paths are processed statistically to determine the probability of detection (POD) of this damage detection method. It was found that the Lamb wave with the driving frequency of f=450  kHz performed best in the crack monitoring. By using an threshold damage index DIth=0.01, the detectable crack sizes a50/50, a90/50, and a90/95 for the case of f=450  kHz are 4.83, 5.79, and 5.92 mm, respectively. Based on the proposed approach, the relations between the damage index and actual crack length and the POD curves can be applicable to a real structure with the same geometry.
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      Assessments of Structural Health Monitoring for Fatigue Cracks in Metallic Structures by Using Lamb Waves Driven by Piezoelectric Transducers

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4269205
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    contributor authorChung-De Chen
    contributor authorYu-Cheng Chiu
    contributor authorYao-Hung Huang
    contributor authorPo-Hao Wang
    contributor authorRong-Der Chien
    date accessioned2022-01-30T22:34:51Z
    date available2022-01-30T22:34:51Z
    date issued1/1/2021
    identifier other(ASCE)AS.1943-5525.0001212.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4269205
    description abstractIn this paper, the assessments of structural health monitoring (SHM) for metallic structures are presented. Tests were conducted on three specimens for fatigue crack testing and damage index measurements. In each specimen, a transducer array of six Stanford Multiactuator-Receiver Transduction (SMART) Layers, each of which contains a piezoelectric transducer, was mounted near the fatigue crack. The Lamb wave was driven by one SMART Layer and received by another. The transducer array generated nine forward and nine backward propagating paths. The damage index defined in the first arrival window (FAW) was obtained for each path. In this work, we propose an averaging process to obtain average damage index from the transducer array. The Lamb waves with various driving frequencies were tested to conduct the performance of the damage monitoring. The results show that the plot of the average damage index versus the actual crack length reveals a narrow band, indicating a small standard deviation of the measurement data. The data of numerous crack lengths and Lamb wave paths are processed statistically to determine the probability of detection (POD) of this damage detection method. It was found that the Lamb wave with the driving frequency of f=450  kHz performed best in the crack monitoring. By using an threshold damage index DIth=0.01, the detectable crack sizes a50/50, a90/50, and a90/95 for the case of f=450  kHz are 4.83, 5.79, and 5.92 mm, respectively. Based on the proposed approach, the relations between the damage index and actual crack length and the POD curves can be applicable to a real structure with the same geometry.
    publisherASCE
    titleAssessments of Structural Health Monitoring for Fatigue Cracks in Metallic Structures by Using Lamb Waves Driven by Piezoelectric Transducers
    typeJournal Paper
    journal volume34
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001212
    journal fristpage04020091
    journal lastpage04020091-10
    page10
    treeJournal of Aerospace Engineering:;2021:;Volume ( 034 ):;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
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