Simulations of pitch-heave limit-cycle oscillations at a transitional reynolds number

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.2514/1.J052225
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Affiliation
  1. National Research Council of Canada. Aerospace
  2. National Research Council of Canada
FormatText, Article
SubjectAerodynamic damping; Aeroelastic oscillations; Boundary-layer separation; Computational Fluid Dynamics codes; Limit cycle oscillations; Low Reynolds number; Nonlinear feedback coupling; Structural response; Aerodynamics; Airfoils; Computational fluid dynamics; Large eddy simulation; Reynolds number; Aeroelasticity
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LanguageEnglish
Peer reviewedYes
NPARC number21269606
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Record identifierd8b37066-e8d7-4695-b75e-e04b4c09d4fd
Record created2013-12-13
Record modified2020-04-22
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