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Simulation of Trailing Edge Vortex Shedding in a Transonic Turbine Cascade

From National Research Council Canada

AuthorSearch for: 1; Search for: 1
Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
FormatText, Article
ConferenceInternational Gas Turbine and Aeroengine Congress & Exhibition. Birmingham, UK
Access condition
  • available
  • unlimited
In
  • International Gas Turbine and Aeroengine Congress & Exhibition [Proceedings], 96-GT-483.
Peer reviewedYes
NRC numberAL-1996-0020
NPARC number8932714
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Record identifier1bb538c2-099c-44ff-a784-64bd3e36df0e
Record created2009-04-23
Record modified2020-05-08
Date modified: