Effect of freestream turbulence on airfoil limit-cycle oscillations at transitional reynolds numbers

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.2514/1.C032807
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Name affiliation
  1. National Research Council Canada. Aerospace
FormatText
TypeArticle
Journal titleJournal of Aircraft
ISSN0021-8669
Volume52
Issue4
Pages12141225; # of pages: 12
SubjectAirfoils; Boundary layer flow; Boundary layers; Computational fluid dynamics; Laminar boundary layer; Navier Stokes equations; Reynolds number; Shear stress; Turbulence; Boundary-layer separation; Computational Fluid Dynamics codes; Correlation-based transition models; Freestream turbulence intensity; Laminar turbulent transitions; Limit Cycle Oscillation (LCO); National Research Council; Unsteady reynolds-averaged navier-stokes; Atmospheric thermodynamics
Abstract
Publication date
PublisherAmerican Institute of Aeronautics and Astronautics
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LanguageEnglish
Peer reviewedYes
NPARC number21277387
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Record identifier14cba407-cdda-4790-8590-eb3ac2296899
Record created2016-03-09
Record modified2016-05-09
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