Using a simple crack growth model in predicting remaining useful life

Journal of Aircraft

Volumn 49, Issue 6, 2012, Pages 1965-1973

  Coppe, Alexandra ^a   Pais, Matthew J ^a   Haftka, Raphael T ^a   Kim, Nam H ^a  

^a UNIVERSITY OF FLORIDA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BAYESIAN NETWORKS; DAMAGE DETECTION; FATIGUE CRACK PROPAGATION; GEOMETRY; INFERENCE ENGINES; STRESS INTENSITY FACTORS; STRUCTURAL HEALTH MONITORING;

BAYESIAN IDENTIFICATION; BAYESIAN INFERENCE; CRACK GROWTH MODEL; EXTENDED FINITE ELEMENT METHOD; NUMBER OF CYCLES TO FAILURE; REMAINING USEFUL LIVES; SIMPLE PHYSICAL MODELS; STRUCTURAL HEALTH MONITORING SYSTEMS;

CRACKS;

EID: 84871829878     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.C031808     Document Type: Article

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