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Evolution of the surface flow topology on a 65° delta wing and its correspondence to the critical states, AIAA 2000-790

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.2514/6.2000-790
AuthorSearch for: 1; Search for: 1
Affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
FormatText, Article
Conference38th Aerospace Sciences Meeting and Exhibit, January 10-13, 2000, Reno, Nevada, USA
Subjectleading-edge vortex; high angle of attack
PublisherAmerican Institute of Aeronautics and Astronautics
In
  • Aerospace Sciences Meetings: 38th Aerospace Sciences Meeting and Exhibit.
Peer reviewedYes
NRC numberAL-2000-0083
NPARC number8926628
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Record identifierddec058b-9a8d-4c84-99db-437f41281cf4
Record created2009-04-23
Record modified2020-04-16
Date modified: