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

From National Research Council Canada

DOIResolve DOI:
AuthorSearch for: 1; Search for: 1; Search for: 1; Search for: 1; Search for: 1
  1. National Research Council of Canada. Aerospace
FormatText, Article
ConferenceASME Turbo Expo 2014: Turbine Technical Conference and Exposition, GT 2014, 16 June 2014 through 20 June 2014
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
Publication date
Peer reviewedYes
NPARC number21275584
Export citationExport as RIS
Report a correctionReport a correction (opens in a new tab)
Record identifier38b9ef08-59dd-4068-871c-4ea333eb663e
Record created2015-07-14
Record modified2020-04-22
Date modified: