A CFD Approach towards Modeling Blade/Vortex Impingement Effects

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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
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Access conditionavailable
Peer reviewedYes
NRC numberAL-2001-0056
NPARC number8929870
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Record identifier9f999333-503e-4163-96b1-cdf4580aed67
Record created2009-04-23
Record modified2016-05-09
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