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contributor authorJiaqi Zhang
contributor authorZhanjun Wu
contributor authorZhengyan Yang
contributor authorChang Gao
contributor authorKehai Liu
contributor authorYuebin Zheng
contributor authorKai Zhou
date accessioned2022-01-30T20:12:23Z
date available2022-01-30T20:12:23Z
date issued2020
identifier other%28ASCE%29AS.1943-5525.0001134.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4266684
description abstractGuided waves have been widely utilized in various structural health monitoring (SHM) techniques because of their long propagation distance and high sensitivity to small-scale defects in structural types such as plates and bars. In particular, T-bars are typical structural components commonly used in aerospace engineering, playing significant roles in load-carrying. Thus, the health states of T-bars largely affect the integrity and safety of aircraft structures. This paper presents a novel defect-detection method for T-bars relying on the examination of propagation characteristics of multimode guided waves. To select proper wave frequencies and modes that are sensitive to different locations of defects in T-bars, the dispersion curves and cross-sectional mode shapes of multimode guided waves are investigated systematically using the semianalytical finite element (SAFE) method. A defect localization strategy is then developed based on the multimode characteristics, able of identifying defects both along the longitudinal direction and the cross-sectional region. A weighted gathering method is presented to reduce the interference from the modes other than the selected ones, giving rise to increased accuracy of defect identification. Both finite element (FE) simulations and experiments are performed for an aluminum T-bar structure to validate the feasibility and precision of the proposed method.
publisherASCE
titleMultimode Guided Waves–Based Structural Defect Localization Longitudinally and Cross-Sectionally in T-Bars
typeJournal Paper
journal volume33
journal issue4
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0001134
page04020017
treeJournal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 004
contenttypeFulltext


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