A fuel saving way in aerospace engineering based on morphing wing technology: a new multidisciplinary experimental model

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DOIResolve DOI: https://doi.org/10.14621/ce.20160202
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Affiliation
  1. National Research Council of Canada. Aerospace
FormatText, Article
Subjectenergy save; drag reduction; morphing wing; experimental testing; wind tunnel; IR analysis
Abstract
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LanguageEnglish
Peer reviewedYes
NPARC number23000917
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Record identifierac894349-03de-419c-882a-89bc9b664601
Record created2016-11-15
Record modified2020-06-02
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