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Finite Element Based Vibration Analysis of Gas Turbine Engine Blades Damaged in Operation

From National Research Council Canada

AuthorSearch for: 1
Affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
FormatText, Other
PlaceChandler, AZ
Access condition
  • unclassified/unlimited
NRC numberSMPL-1999-0102
NPARC number8934054
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Record identifier49059c92-d6b6-47ca-8a49-eb7088dc03e8
Record created2009-04-23
Record modified2020-03-03
Date modified: