High-velocity impact location on aircraft panels using macro-fiber composite piezoelectric rosettes

Journal of Intelligent Material Systems and Structures

Volumn 21, Issue 9, 2010, Pages 887-896

  Salamone, Salvatore ^a   Bartoli, Ivan ^a   Di Leo, Patrizia ^b   Lanza Di Scalea, Francesco ^a   Ajovalasit, Augusto ^b   D'Acquisto, Leonardo ^b   Rhymer, Jennifer ^a   Kim, Hyonny ^a  

^a UNIVERSITY OF CALIFORNIA   (United States)

^b UNIVERSITY OF PALERMO   (Italy)

Author keywords

Acoustic emissions; Impact location; Macro fiber composite transducers; Structural health monitoring

Indexed keywords

AIRCRAFT PANELS; ANISOTROPIC MATERIAL; COMPOSITE AIRCRAFT; DIRECTIVITY; GAS GUN; HIGH-VELOCITY IMPACT; MACRO FIBER COMPOSITE; MACRO-FIBER COMPOSITE TRANSDUCERS; PRINCIPAL STRAIN; TIME OF FLIGHT; WAVE DIRECTION; WAVE SPEED;

ACOUSTIC EMISSION TESTING; ACOUSTIC EMISSIONS; FIBERS; MICROBIAL FUEL CELLS; PIEZOELECTRICITY; STRUCTURAL HEALTH MONITORING; STRUCTURAL MEMBERS; TRIANGULATION;

ACOUSTIC TRANSDUCERS;

EID: 77952983228     PISSN: 1045389X     EISSN: 15308138     Source Type: Journal    
DOI: 10.1177/1045389X10368450     Document Type: Article

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