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

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DOIResolve DOI: https://doi.org/10.1016/j.ast.2016.03.014
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Name affiliation
  1. National Research Council Canada. Aerospace
FormatText
TypeArticle
Journal titleAerospace Science and Technology
ISSN1270-9638
Subjectmorphing wing; morphing aileron; CFD; infra-red tests; wind tunnel tests; laminar-to-turbulent flow transition
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PublisherElsevier
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LanguageEnglish
Peer reviewedYes
NPARC number21277526
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Record identifier8ed03609-076e-4361-aaf3-778dc292de75
Record created2016-03-31
Record modified2019-03-06
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