Aerostructural model for morphing laminar wing optimization in a wind tunnel

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.2514/1.C000232
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Affiliation
  1. National Research Council of Canada. Aerospace
FormatText, Article
SubjectActive structures; Angles of attack; Drag forces; Finite element software; Flight conditions; Flow condition; Infrared thermography; Local search; Morphing; Numerical models; Numerical results; Optimization algorithms; Tunnel measurements; Wind-tunnel testing; Wing chord; Wing surface; Aerodynamics; Computer software; Drag; Laminar flow; Mach number; Optimization; Wind tunnels
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LanguageEnglish
Peer reviewedYes
NPARC number21271386
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Record created2014-03-24
Record modified2020-04-21
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