Quantitative Structural Health Monitoring by Ultrasonic Guided Waves
Publication: Journal of Engineering Mechanics
Volume 136, Issue 8
Abstract
This paper presents a global-local (GL) method to simulate the interaction of ultrasonic guided waves with structural defects in isotropic and multilayered composite platelike structures. The GL method uses a full finite-element (FE) discretization of the defected region to properly represent wave diffraction phenomena and a suitable set of wave functions to simulate regions away from the joint. Displacement and stress continuity conditions are imposed at the boundary between the global and the local regions. The radiated wave field can be then calculated by using standard techniques (least-squares method). The novelty of the proposed approach over previous GL techniques is the use of semianalytical FE (SAFE) modeling for the “global” simulation. The SAFE method, which only requires the discretization of the waveguide’s cross section, allows handling complex structures (multilayered composites, arbitrary cross sections, etc.) in a computationally efficient manner. Applications of the GL method to damage quantification will be shown for the cases of notches in aluminum plates and delaminationlike defects in aircraft composite panels.
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Acknowledgments
This project was funded by (U.S.) Air Force Office of Scientific Research Contract No. USAFOSRFA9550-07-1-0016 (Dr. Victor Giurgiutiu and David Stargel, Program Managers) and by the Los Alamos/UCSD Education Collaboration Task 2 “Structural Integrity Monitoring of UAV Composite Wings.” Dr. Ivan Bartoli is acknowledged for preparing Fig. 2.
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© 2010 ASCE.
History
Received: Apr 22, 2008
Accepted: Jan 2, 2010
Published online: Jan 6, 2010
Published in print: Aug 2010
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