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Volumn 11, Issue 6, 2012, Pages 671-683
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Predictive modeling of electromechanical impedance spectroscopy for composite materials
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Author keywords
composite materials; Electromechanical impedance spectroscopy; finite element modeling; piezoelectric wafer active sensors; structural health monitoring
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Indexed keywords
AIRCRAFT STRUCTURE;
BONDING LAYERS;
DAMAGE MODEL;
ELECTROMECHANICAL BEHAVIOR;
ELECTROMECHANICAL CONVERSION;
ELECTROMECHANICAL IMPEDANCE;
EXPERIMENTAL VALIDATIONS;
FINITE ELEMENT MODELING;
GLASS-FIBER REINFORCED POLYMER COMPOSITES;
HOST STRUCTURE;
IMPEDANCE RESPONSE;
INPUT AND OUTPUTS;
LAMINATED GLASS;
LOW AND HIGH FREQUENCIES;
ORTHOTROPIC STRUCTURE;
PIEZOELECTRIC WAFER ACTIVE SENSORS;
PIEZOELECTRIC WAFERS;
PREDICTIVE MODELING;
SELF-SENSING;
STRUCTURAL HEALTH MONITORING TECHNOLOGY;
AIRCRAFT MANUFACTURE;
AIRFRAMES;
COMPOSITE MATERIALS;
COMPOSITE STRUCTURES;
FIBER REINFORCED PLASTICS;
FINITE ELEMENT METHOD;
GLASS FIBERS;
PIEZOELECTRICITY;
SENSORS;
STRUCTURAL HEALTH MONITORING;
WAFER BONDING;
SPECTROSCOPY;
AIR CRAFT;
CHIPS;
COMPOSITES;
FINITE ELEMENT ANALYSIS;
GLASS FIBERS;
MATHEMATICAL MODELS;
PIEZOELECTRICITY;
REINFORCED PLASTIC;
SENSORS;
SPECTROSCOPY;
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EID: 84868712080
PISSN: 14759217
EISSN: 17413168
Source Type: Journal
DOI: 10.1177/1475921712451954 Document Type: Article |
Times cited : (99)
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References (22)
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