Numerical simulation and wind tunnel tests investigation and validation of a morphing wing-tip demonstrator aerodynamic performance

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  1. National Research Council of Canada. Aerospace
FormatText, Article
Subjectmorphing wing; morphing aileron; CFD; infra-red tests; wind tunnel tests; laminar-to-turbulent flow transition
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Peer reviewedYes
NPARC number21277526
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Record identifier8ed03609-076e-4361-aaf3-778dc292de75
Record created2016-03-31
Record modified2020-06-04
Date modified: