Principal component analysis of acoustic emission signals from landing gear components: An aid to fatigue fracture detection

Strain

Volumn 47, Issue SUPPL. 1, 2011, Pages

  Eaton, M J ^a   Pullin, R ^a   Hensman, J J ^b   Holford, K M ^a   Worden, K ^b   Evans, S L ^a  

^a CARDIFF UNIVERSITY   (United Kingdom)

^b UNIVERSITY OF SHEFFIELD   (United Kingdom)

Author keywords

acoustic emission; aerospace; fracture detection; principal component analysis

Indexed keywords

ACOUSTIC EMISSION SIGNAL; AE SIGNALS; AEROSPACE; ARTIFICIAL SOURCES; BACKGROUND NOISE; FATIGUE FRACTURE; FRACTURE DETECTION; LOAD CONDITION; NO LOAD; PRINCIPAL COMPONENTS; SOURCE TYPES;

ACOUSTIC EMISSION TESTING; ACOUSTIC EMISSIONS; ACOUSTIC NOISE; CRACK DETECTION; CRACKS; FATIGUE CRACK PROPAGATION; FATIGUE OF MATERIALS; FATIGUE TESTING; FRACTURE; FRACTURE TESTING; LANDING; LANDING GEAR (AIRCRAFT); SIGNAL DETECTION; ULTRASONIC APPLICATIONS;

PRINCIPAL COMPONENT ANALYSIS;

EID: 79958813541     PISSN: 00392103     EISSN: 14751305     Source Type: Journal    
DOI: 10.1111/j.1475-1305.2009.00661.x     Document Type: Article

References (7)

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