The use of vortex generators to delay boundary layer separation: theoretical discussion supported by tests on a CF-100 aircraft

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DOIResolve DOI: http://doi.org/10.4224/23001523
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TypeTechnical Report
Series titleNational Aeronautical Establishment (Canada) Laboratory report LR; no. LR-183
Physical description44, [55] p.
Publication date
PublisherNational Research Council Canada. Division of Mechanical Engineering. National Aeronautical Establishment
LanguageEnglish
AffiliationNational Research Council Canada
Peer reviewedNo
NPARC number23001523
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Record identifierfac4ad3f-0f25-4a93-821d-4eb4640c693b
Record created2017-02-28
Record modified2017-03-27
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