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Transition Prediction in Low Reynolds Airfoil Flows using Finite Element/Difference Solvers Coupled with the en Method: A Comparative Study

From National Research Council Canada

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Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
  2. Institute of Fluid Mechanics, Braunschweig Technical University, 38106 Braunschweig
FormatText, Article
ConferenceAIAA 24th Applied Aerodynamics Conference (from 6/4/2006 to 6/8/2006), San Francisco
Subjecttransition; HGR-01; airfoil; incompressible; finite element
Access condition
  • available
  • unclassified
  • unlimited
Peer reviewedYes
NRC numberAL-2006-0129
NPARC number8928231
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Record identifier5e6a43ed-e525-4d30-be01-4e1db2ccc4b3
Record created2009-04-23
Record modified2020-04-16
Date modified: