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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 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: