A new algorithm for acoustic emission localization and flexural group velocity determination in anisotropic structures

Composites Part A: Applied Science and Manufacturing

Volumn 41, Issue 12, 2010, Pages 1777-1786

  Ciampa, F ^a   Meo, M ^a  

^a University of Bath   (United Kingdom)

Author keywords

A. Carbon fibre; A. Honeycomb; D. Acoustic emission; D. Non destructive testing

Indexed keywords

A. HONEYCOMB; ANISOTROPIC STRUCTURE; CARBON FIBRES; COMPUTATIONAL TIME; CONTINUOUS WAVELET TRANSFORMS; D. ACOUSTIC EMISSION; EMISSION LOCALIZATION; EXPERIMENTAL TEST; FLEXURAL WAVE; GROUP SPEED; GROUP VELOCITIES; IMPACT SOURCE LOCATION; IN-SITU; LAMB MODES; LINE SEARCHES; LOW VELOCITY IMPACT; MAXIMUM ERROR; NON DESTRUCTIVE TESTING; PIEZOELECTRIC SENSORS; REASONABLE ACCURACY; SANDWICH PANEL; SANDWICH PLATES; STRESS WAVE; TIME OF ARRIVAL;

ACOUSTIC EMISSION TESTING; ACOUSTIC EMISSIONS; ALGORITHMS; CARBON FIBERS; ELASTIC WAVES; HONEYCOMB STRUCTURES; LIGHT VELOCITY; STRUCTURE (COMPOSITION); WAVE EQUATIONS; WAVE PROPAGATION; WAVELET TRANSFORMS;

STRUCTURAL HEALTH MONITORING;

EID: 77958088639     PISSN: 1359835X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compositesa.2010.08.013     Document Type: Article

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