Topology of the flow on a 65° delta wings

From National Research Council Canada

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Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
FormatText, Book Chapter
Subjectflow topology; leading-edge vortex; vortex breakdown; slender wing; wind tunnel experiments; flow visualisation; topology; delta wing; vortices
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PublisherNATO Science and Technology Organization
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LanguageEnglish
Peer reviewedYes
NRC numberAL-2007-0106
NPARC number8931937
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Record identifier1231a1aa-5292-4212-b6f1-2f01db353762
Record created2009-04-23
Record modified2020-06-17
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