Smart monitoring of aeronautical composites plates based on electromechanical impedance measurements and artificial neural networks

Engineering Structures

Volumn 56, Issue , 2013, Pages 794-804

  Selva, Pierre ^a   Cherrier, Olivier ^b   Budinger, Valérie ^c   Lachaud, Frédéric ^b   Morlier, Joseph ^b  

^a CT Ingénierie   (France)

^b UNIVERSITÉ DE TOULOUSE   (France)

^c INSA   (France)

Author keywords

Composite structures; EM impedance; Neural networks; Structural health monitoring

Indexed keywords

CARBON FIBER REINFORCED; DAMAGED STRUCTURES; DETECTION AND LOCALIZATION; ELECTROMECHANICAL IMPEDANCE; ELECTROMECHANICAL IMPEDANCE TECHNIQUES; HIGH FREQUENCY HF; LAMINATED COMPOSITE PLATES; STRUCTURAL HEALTH MONITORING (SHM);

COMPOSITE STRUCTURES; DAMAGE DETECTION; LAMINATED COMPOSITES; PLATES (STRUCTURAL COMPONENTS); PRINCIPAL COMPONENT ANALYSIS; STRUCTURAL HEALTH MONITORING;

NEURAL NETWORKS;

ARTIFICIAL NEURAL NETWORK; COMPOSITE; COMPUTER SIMULATION; DAMAGE MECHANICS; FINITE ELEMENT METHOD; MECHANICAL PROPERTY; PRINCIPAL COMPONENT ANALYSIS; STRUCTURAL ANALYSIS;

EID: 84880437231     PISSN: 01410296     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.engstruct.2013.05.025     Document Type: Article

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