Transducer Placement Option of Lamb Wave SHM System for Hotspot Damage Monitoring - Ewald, Vincentius; Groves, Roger M.; Benedictus, Rinze (Aerospace, 2018)
Keywords: additive color model; Aircraft; Aircraft detection; Aircraft structures; Airframes; Algorithms; Aluminum; Centroids; Computer vision; Crack propagation; Damage detection; Damage tolerance; Fatigue cracks; Fatigue failure; Finite element method; finite element modelling; Fracture mechanics; Fuselages; hotspot damage; Image analysis; image processing; Lamb wave; Lamb waves; Optimization; Performance assessment; Placement; Position measurement; Position sensing; Propagation; sensor placement option; Sensors; Simulation; Structural health monitoring; Structural Health Monitoring (SHM); Wave propagation