Open Access
Mechanics & Industry
Volume 21, Number 6, 2020
Article Number 620
Number of page(s) 8
Published online 21 December 2020
  1. T. Kinsey, G. Dumas, G. Lalande, J. Ruel, A. Mehut, P. Viarouge, J. Lemay, Y. Jean, Prototype testing of a hydrokinetic turbine based on oscillating hydrofoils. Renew. Energy 36, 1710–1718 (2011) [Google Scholar]
  2. M. Gaster, The structure and behaviour of laminar separation bubbles. Aeronautical Research Council Reports and Memoranda-Report No 3595 (1967) [Google Scholar]
  3. O. Marxen, D.S. Henningson, The effect of small-amplitude convective disturbances on the size and bursting of a laminar separation bubble. J. Fluid Mech. 671, 1–33 (2011) [Google Scholar]
  4. A. Roshko, On the development of turbulent wakes from vortex streets. Tech. rep., National Advisory Committee for Aeronautics. Tech Note 2913. California Institute of Technology (1954) [Google Scholar]
  5. C.H. Williamson, Vortex dynamics in the wake of a cylinder. In Fluid vortices. Springer (1995) 155–234 [CrossRef] [Google Scholar]
  6. B. Carmichael, Low reynolds number airfoil survey, volume 1. Tech. rep., NASA, contrator Report 165803 (1981) [Google Scholar]
  7. P. Lissaman, Low-reynolds-number airfoils. Annu. Rev. Fluid Mech. 15, 223–239 (1983) [Google Scholar]
  8. P. Balakumar, Direct numerical simulation of flows over an naca-0012 airfoil at low and moderate reynolds numbers. In 47th AIAA Fluid Dynamics Conference (2017), p. 3978 [Google Scholar]
  9. L.B. Streher, Large-eddy simulation of the flow around a naca-0012 airfoil at different amgles of attack. Master’s thesis, Helmut Schmidt University, 2017 [Google Scholar]
  10. D. Poirel, Y. Harris, A. Benaissa, Self-sustained aeroelastic oscillations of a naca0012 airfoil at low-to-moderate Reynolds numbers. J. Fluids Struct. 24, 700–719 (2008) [Google Scholar]
  11. C.J. Barnes, M.R. Visbal, On the role of flow transition in laminar separation flutter. J. Fluids Struct. 77, 213–230 (2018) [Google Scholar]
  12. A. Poels, D. Rudmin, A. Benaissa, D. Poirel, Localization of flow separation and transition over a pitching naca0012 airfoil at transitional reynolds numbers using hot-films. J. Fluids Eng. 137, 124501 (2015) [Google Scholar]
  13. D. Poirel, Y. Harris, A. Benaissa, Aeroelastic dynamics of a naca 0012 airfoil in the transitional reynolds number regime. In ASME 2006 Pressure Vessels and Piping/ICPVT-11 Conference, American Society of Mechanical Engineers (2006) 847–854 [CrossRef] [Google Scholar]
  14. B. McGranahan, M. Selig, Surface oil flow measurements on several airfoils at low Reynolds numbers. In 21st AIAA Applied Aerodynamics Conference (2003) 4067 [Google Scholar]
  15. D. Rudmin, Detection of laminar flow separation and transition on a piching naca0012 airfoil. Master’s thesis, Mechanical and Aerospace Engineering, Royal Military College of Canada (2012) [Google Scholar]
  16. D. Rudmin, A. Benaissa, D. Poirel, Detection of laminar flow separation and transition on a naca-0012 airfoil using surface hot-films. J. Fluids Eng. 135, 101104 (2013) [Google Scholar]
  17. H.-W. Lee, R.-F. Huang, Frequency selection of wake flow behind a naca 0012 wing. J. Mar. Sci. Technol. 6, 29–37 (1998) [Google Scholar]
  18. R.F. Huang, C.L. Lin, Vortex shedding and shear-layer instability of wing at low-Reynolds numbers. AIAA J. 33, 1398–1403 (1995) [Google Scholar]
  19. R.F. Huang, H.W. Lee, Effects of freestream turbulence on wing-surface flow and aerodynamic performance. J. Aircraft 36, 965–972 (1999) [CrossRef] [Google Scholar]
  20. Y. Jung, S.O. Park, Vortex-shedding characteristics in the wake of an oscillating airfoil at low reynolds number. J. Fluids Struct. 20, 451–464 (2005) [Google Scholar]

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