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The Influence of Reynolds Number, Turbulence Intensity and Length Scale on Separated-Flow Transition of a Low-Pressure Turbine Airfoil

From National Research Council Canada

AuthorSearch for: 1; Search for: 1; Search for: 2
Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
  2. Carleton University
FormatText, Article
ConferenceASME TurboExpo 2004 from June 14, 2004 to June 17, 2004, Vienna, Austria
SubjectHigh-lift low-pressure turbine blade; Transition; Low Reynolds number; Laminar separation
Access condition
  • available
  • unclassified
  • unlimited
Peer reviewedYes
NRC numberAL-2003-0076
NPARC number8932709
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Record identifiera7eadb11-2d8a-47ef-86ec-4a8521484aed
Record created2009-04-23
Record modified2020-04-16
Date modified: