Detection and monitoring of hidden fatigue crack growth using a built-in piezoelectric sensor/actuator network: II. Validation using riveted joints and repair patches

By Jeong-Beom Ihn, Fu-Kuo Chang. 2004

245 citations recorded by the source corpus.

Subfields: Civil and Structural Engineering, Mechanical Engineering, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/5c91de49e3241800df0d6fb4df5b1b80a9f6e2e7

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In Civil and Structural Engineering

In Mechanical Engineering

In Mechanics of Materials

Citations in the corpus

Active health monitoring of an aircraft wing with embedded piezoelectric sensor/actuator network: I. Defect detection, localization and growth monitoring (2007, methodology): “Keilers and Chang [7], Ihn and Chang [8, 9] and Yang and Chang [10, 11] used the built-in piezoelectric transducers for delamination identification in composite plates, fatigue crack detection and growth monitoring in riveted lap joints and repair patches, and bolt joint loosening inspection in comp”
Energy Harvesting for Structural Health Monitoring Sensor Networks (2008, background): “Many of the features identified for impedance-based and wave propagation-based SHM studies fall into this category [5, 6, 7, 8].”
Damage detection sensitivity characterization of acousto-ultrasound-based structural health monitoring techniques (2016, methodology): “More specifically, in this study we address the effects of the following: (1) sensor, structural, and adhesive material property variations on the DI; (2) uncertainty in the sensor installation on the DI including both the variation in the adhesive thickness and the location of the sensors; and (3) ”
Performance assessment and validation of piezoelectric active-sensors in structural health monitoring (2006, background): “collectively such as smart layer networks ( Ihn and Chang 2004 ), or the sensors (such as PVDF) can cover”
Pitch-catch Active Sensing Methods in Structural Health Monitoring for Aircraft Structures (2008, methodology): “Accordingly, by selecting appropriate Lamb wave modes from the receiving sensor measurements, the following damage indices were proposed by the authors [8,9] to quantify crack and debond size:”