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

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  1. National Research Council of Canada
FormatText, Technical Report
Physical description44, [55] p.
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PublisherNational Research Council of Canada. Division of Mechanical Engineering. National Aeronautical Establishment
Peer reviewedNo
NPARC number23001523
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Record identifierfac4ad3f-0f25-4a93-821d-4eb4640c693b
Record created2017-02-28
Record modified2022-07-26
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