Impact identification of stiffened composite panels: I. System development

By R. Seydel, Fu-Kuo Chang. 2001

188 citations recorded by the source corpus.

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Acoustic emission source localization and velocity determination of the fundamental mode A0 using wavelet analysis and a Newton-based optimization technique (2010, unknown): “Seydel and Chang (2001) proposed an approach based on a double peak method wherein the arrival time was chosen by selecting the minimum before the maximum for each signal.”
Piezoelectric Transducer-Based Structural Health Monitoring for Aircraft Applications (2019, methodology): “conducted an investigation to develop an impact identification system for the prediction of force location and history of low-velocity impact on the stiffened plate [130,131].”
Structural Damage Location with Fiber Bragg Grating Rosettes and Lamb Waves (2007, background): “, system modeling [12,13] and artificial neural networks [14,15].”
Built-in Sensor Network for Structural Health Monitoring of Composite Structure (2007, methodology): “In passive sensing mode, the piezoelectric sensors are used as continuously monitored sensors that ‘listen’ for external impact events (Seydel and Chang, 2001).”