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

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TypeArticle
ConferenceAIAA 24th Applied Aerodynamics Conference (from 6/4/2006 to 6/8/2006), San Francisco
Subjecttransition; HGR-01; airfoil; incompressible; finite element
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Access conditionavailable
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 modified2016-05-09
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