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: https://doi.org/10.1016/j.cja.2016.12.018
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Name affiliation
  1. National Research Council of Canada. Aerospace
FormatText, Article
Subjectdrag reduction; infra-red tests; morphing wing; optimization; wind tunnel test
Publication date
Peer reviewedYes
NPARC number23001243
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Record identifierffa11266-d9f4-4762-9715-ae85ba0ed8af
Record created2017-01-11
Record modified2020-06-02
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