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Unsteady Flows past Oscillating Airfoil Using Chimera Grid Technique

From National Research Council Canada

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Affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
FormatText, Article
ConferenceCASI 9th Aerodynamica Symposium 2003 ( April 28 to 30, 2003), Montreal, Canada
Subjectchimera; unsteady; structured grid
Access condition
  • available
  • unclassified
  • unlimited
Peer reviewedYes
NRC numberAL-2002-0103
NPARC number8933626
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Record identifierc356bfdd-35ea-4cc7-a887-9b5683d64db9
Record created2009-04-23
Record modified2020-04-16
Date modified: