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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  1. National Research Council of Canada. Aerospace
FormatText, Article
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
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Peer reviewedYes
NPARC number21277387
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Record identifier14cba407-cdda-4790-8590-eb3ac2296899
Record created2016-03-09
Record modified2020-04-22
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