Residual life assessment of a critical component of a gas turbine-achievements and challenges

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1115/GT2014-26423
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Name affiliation
  1. National Research Council Canada. Aerospace
FormatText
TypeArticle
Proceedings titleProceedings of the ASME Turbo Expo
ConferenceASME Turbo Expo 2014: Turbine Technical Conference and Exposition, GT 2014, 16 June 2014 through 20 June 2014
ISBN9780791845769
Volume7A
SubjectCrack propagation; Cracks; Damage detection; Engines; Fatigue crack propagation; Fatigue of materials; Finite element method; Fracture; Numerical methods; Uncertainty analysis; Economic operations; Experimental validations; Mixed-mode interactions; Safety critical components; Scanning electronic microscopy; Striation formation; Threedimensional (3-d); Weight function method; Gas turbines
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LanguageEnglish
Peer reviewedYes
NPARC number21275584
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Record identifier38b9ef08-59dd-4068-871c-4ea333eb663e
Record created2015-07-14
Record modified2016-05-09
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