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The Aerodynamics of a Low-Pressure Turbine Airfoil under Periodically Unsteady Conditions

From National Research Council Canada

AuthorSearch for: 1; Search for: 2
Affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
  2. Carleton University
FormatText, Article
ConferenceASME Turbo Expo 2004 from June 6, 2004 to June 17, 2004, Vienna, Austria
SubjectHigh-lift low-pressure turbine blade; Transition; Unsteady aerodynamics; low Reynolds number; Laminar separation
Access condition
  • available
  • unclassified
  • unlimited
Peer reviewedYes
NRC numberAL-2003-0077
NPARC number8927373
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Record identifierd697cfc3-edeb-46ce-acdd-ae25a0e8536b
Record created2009-04-23
Record modified2020-04-16
Date modified: