Experimental and computational investigations of flapping wings for Nano-air-vehicles

From National Research Council Canada

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DOIResolve DOI: https://doi.org/10.1080/19942060.2015.1004820
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Affiliation
  1. National Research Council of Canada. Aerospace
FormatText, Article
SubjectFlapping wing; Low Reynolds number flow; Micro air vehicle; Water tunnel; Computational fluid dynamics
Abstract
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PublisherTaylor & Francis
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LanguageEnglish
Peer reviewedYes
NPARC number23000259
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Record identifier72e8bec0-4a62-4ee9-887e-ad10d42a2920
Record created2016-06-29
Record modified2020-06-02
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