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A CFD Approach towards Modeling Blade/Vortex Impingement Effects

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
ConferenceThe 23rd Congress of The International Council of the Aeronautical Sciences (ICAS) from 09/08/2002 to 09/13/2002, Toronto
SubjectBGK airfoil; shock oscillation; shock tube; airfoil-vortex-interaction
Access condition
  • available
  • unclassified
  • unlimited
Peer reviewedYes
NRC numberAL-2001-0056
NPARC number8929870
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Record identifier9f999333-503e-4163-96b1-cdf4580aed67
Record created2009-04-23
Record modified2020-04-16
Date modified: