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All issues Volume 114 (2016) EPJ Web of Conferences, 114 (2016) 02016 References
Open Access
Issue
EPJ Web of Conferences
Volume 114, 2016
EFM15 – Experimental Fluid Mechanics 2015
Article Number 02016
Number of page(s) 5
Section Contributions
DOI https://doi.org/10.1051/epjconf/201611402016
Published online 28 March 2016
  1. W. Zhang, R. Hain, C.J. Kahler, Scanning PIV investigation of the laminar separation bubble on a SD7003 airfoil. Exp. Fluids. 45(4), 725-743 (2008) [CrossRef] [Google Scholar]
  2. R. Ricci, S.A. Montelpare, Quantitative IR thermographic method to study the laminar separation bubble phenomenon. Int J Therm Sci. 44(8), 709-719 (2005) [CrossRef] [Google Scholar]
  3. M.S. Genc, Numerical Simulation of Flow over a Thin Aerofoil at High Re Number using a Transition Model. Proc IMechE, Part C-J Mech Eng Sci, 224(10), 2155-2164 (2010) [CrossRef] [Google Scholar]
  4. M.S. Genc, I. Karasu, H.H. Acıkel, An experimental study on aerodynamics of NACA2415 aerofoil at low Re numbers. Exp Therm Fluid Sci. 39, 252-264 (2012) [CrossRef] [Google Scholar]
  5. M.S. Genc, I. Karasu, H.H. Acıkel, M.T. Akpolat, Low Reynolds number flows and transition, in: M. Serdar Genc (Ed.), Low Reynolds Number Aerodynamics and Transition, Intech-Sciyo Publishing, ISBN 979-953-307-627-9 (2012) [Google Scholar]
  6. M.S. Genc, U. Kaynak, H. Yapıcı, Performance of transition model for predicting low Re aerofoil flows without/with single and simultaneous blowing and suction. Eur J Mech B-Fluid. 30(2), 218-235 (2011) [CrossRef] [Google Scholar]
  7. M.S. Genc, U. Kaynak, G.D. Lock, Flow over an Aerofoil without and with Leading Edge Slat at a Transitional Reynolds Number. Proc IMechE, Part G: J Aerospace Eng. 223(3), 217-231 (2009) [CrossRef] [Google Scholar]
  8. D. Lengani, D. Simoni, M. Ubaldi, P. Zunino, F. Bertini, Turbulent boundary layer separation control and loss evaluation of low profile vortex generators. Exp Therm Fluid Sci. 35(8), 1505-1513 (2011) [CrossRef] [Google Scholar]
  9. M.S. Genç, Unsteady aerodynamics and flowinduced vibrations of a low aspect ratio rectangular membrane wing with excess length. Exp. Therm Fluid Sci. 44, 749-759 (2013) [CrossRef] [Google Scholar]
  10. P. Rojratsirikul, M.S. Genc, Z. Wang, I. Gursul, Flow-induced vibrations of low aspect ratio rectangular membrane wings. J Fluid Struct. 27, 1296-1309 (2011) [CrossRef] [Google Scholar]
  11. G.E. Torres, T.J. Mueller, Low aspect ratio aerodynamics at low Reynolds numbers. AIAA journal. 42(5), 865-873 (2004) [CrossRef] [Google Scholar]
  12. A. Pelletier, T.J. Mueller, Low Reynolds number aerodynamics of low-aspect-ratio, thin/flat/camberedplate wings. J Aircraft. 37(5), 825-832 (2000) [CrossRef] [Google Scholar]
  13. P. Freymuth, W. Bank, F. Finaish, Further visualization of combined wing tip and starting vortex systems. AIAA journal. 25(9), 1153-1159 (1987) [CrossRef] [Google Scholar]
  14. P.H. Cosyn, J. Vierendeels. Numerical investigation of low-aspect-ratio wings at low Reynolds numbers. J Aircraft. 43(3), 713-722 (2006) [CrossRef] [Google Scholar]
  15. R. Wahidi, W. Lai, J.P. Hubner, A. Lang. Volumetric three-component velocimetry and PIV measurements of Laminar Separation Bubbles on a NACA4412 Airfoil. 16th Int. Symp of Applications of Laser Techniques of Fluid Mechanics. Lisbon, Portugal. 09-12 July, (2012) [Google Scholar]
  16. M. Agrawal, G. Saxena, Analysis of wings using airfoil NACA4412 at different angle of attack. IJMER. 3, 1467–1469 (2013) [Google Scholar]
  17. I. Karasu, M.S. Genç, H.H. Açikel, Numerical study on low Reynolds number flows over an Aerofoil. J. Appl. Mech. Eng. 2, 131 (2013) [Google Scholar]
  18. I. Karasu, Experimental and numerical investigations of transition to turbulence and laminar separation bubble over aerofoil at low Reynolds number flows. Graduate School of Natural and Applied Sciences, Erciyes University, Kayseri, Turkey (2011) [Google Scholar]
  19. Werzkirch, Flow Visualization, Academic Press Inc. Ltd., London, (1974) [Google Scholar]
  20. D.F. Perrens, Flow visualisation in low speed wind tunnels. Phys. Educ. 5 (5), 262–265 (1970) [CrossRef] [Google Scholar]

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