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Gas turbine blade stress analysis and mode shape determination using thermoelastic methods

From National Research Council Canada

AuthorSearch for: 1; Search for: 2
Affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
  2. National Research Council Canada. Administrative Services and Property Management
FormatText, Article
ConferenceBritish Society for Strain Measurement International Conference on Advances in Experimental Mechanics, September 9-11 2008, The National Physical Laboratory (NPL), London, UK
Subjectthermoelasticity; differential infrared thermography; vibration; turbine blade
Access condition
  • unclassified
  • unlimited
Peer reviewedYes
NRC numberSMPL-2008-0111
NPARC number8927068
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Record identifier550fd874-ec35-4b33-9872-82cbd444a67b
Record created2009-04-23
Record modified2020-05-08
Date modified: