Optimization and design of a morphing wing tip aircraft demonstrator for drag reduction at low speeds, Part II – Experimental validation using infra-red transition measurements during wind tunnel tests

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DOIResolve DOI: http://doi.org/10.1016/j.cja.2016.12.018
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TypeArticle
Journal titleChinese Journal of Aeronautics
ISSN1000-9361
Subjectdrag reduction; infra-red tests; morphing wing; optimization; wind tunnel test
Abstract
Publication date
PublisherScienceDirect
LanguageEnglish
AffiliationAerospace; National Research Council Canada
Peer reviewedYes
NPARC number23001243
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Record identifierffa11266-d9f4-4762-9715-ae85ba0ed8af
Record created2017-01-11
Record modified2017-01-11
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