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Unsteady Flows Past Two Airfoils in Tandem and Airfoil-Vortex Interaction

From National Research Council Canada

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Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
FormatText, Article
Subjectairfoils in tandem; shock wave; airfoil-vortex-interaction
Access condition
  • available
  • unclassified
  • unlimited
In
  • Journal of Canadian Aeronautics and Space Institute.
NRC numberAL-2001-0058
NPARC number8933264
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Record identifier83689028-4121-4dfd-b179-54a69d534159
Record created2009-04-23
Record modified2020-04-16
Date modified: