Open Access
Volume 39, Number 3, June 2021
Page(s) 668 - 674
Published online 09 August 2021
  1. Leishman G J. Principles of helicopter aerodynamics with CD extra[M]. Cambridge: Cambridge University Press, 2006 [Google Scholar]
  2. Sahin M, Sankar L N, Chandrasekhara M S, et al. Dynamic stall alleviation using a deformable leading edge concept-a numerical study[J]. Journal of Aircraft, 2003, 40 (1): 77– 85 [Article] [CrossRef] [Google Scholar]
  3. Bain J J, Sankar L N, Prasad J V R, et al. Computational modeling of variable-droop leading edge in forward flight[J]. Journal of Aircraft, 2009, 46 (2): 617– 626 [Article] [CrossRef] [Google Scholar]
  4. Chandrasekhara M S. Optimum gurney flap height determination for "lost-lift" recovery in compressible dynamic stall control[J]. Aerospace Science and Technology, 2010, 14 (8): 551– 556 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  5. Johnson C, Barakos G. Optimising aspects of rotor blades in forward flight[C]//49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2011: 1194 [Google Scholar]
  6. Geissler W, Dietz G, Mai H, et al. Dynamic stall control investigations on a full size chord blade section[C]//30th European Rotorcraft Forum, Marseilles France, 2002 [Google Scholar]
  7. Yang Huiqiang, Xu Heyong, Ye Zhengyin. Study on the flow control of the dynamic stall using the co-flow jet[J]. Advances in Aeronautical Science and Engineering, 2018 (4): 16 [Article](in chinese) [Google Scholar]
  8. Xu Jianhua, Li Kai, Song Wenping, et al. influence of co-flow jet key parameters on airfoil aerodynamic performance at low Reynolds numbers[J]. Acta Aeroelastic et Astronautica Sinica, 2018, 39 (8): 88– 102 [Article](in chinese) [Google Scholar]
  9. Durrani N, Haider B A. Study of stall delay over a generic airfoil using synthetic jet actuator[C]//49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 2011: 943 [Google Scholar]
  10. Bai Junqiang, Xin Liang, Liu Nan, et al. Numerical simulation of separation control for high Lift system using distributed zero-net mass flux jet[J]. Journal of Northwestern Polytechnical University, 2015, 32 (2): 188– 194 [Article](in chinese) [Google Scholar]
  11. Zhang P F, Yan B, Dai C F. Lift enhancement method by synthetic jet circulation control[J]. Science China Technological Sciences, 2012, 55 (9): 2585– 2592 [Article] [NASA ADS] [CrossRef] [Google Scholar]
  12. Hao Lishu, Qiao Zhide, Song Wenping. Experimentally studying effects of different layouts of vortex generator on controlling stall flow over airfoil[J]. Journal of Northwestern Polytechnical University, 2011, 29 (4): 524– 528 [Article](in chinese) [Google Scholar]
  13. Vu N A, Lee J W, Shu J I. Aerodynamic design optimization of helicopter rotor blades including airfoil shape for hover performance[J]. Chinese Journal of Aeronautics, 2013, 26 (1): 1– 8 [Article] [CrossRef] [Google Scholar]
  14. Gumerov N A, Duraiswami R. Fast radial basis function interpolation via preconditioned Krylov iteration[J]. SIAM Journal on Scientific Computing, 2007, 29 (5): 1876– 1899 [Article] [CrossRef] [Google Scholar]
  15. Stoll P, Gerlinger P, Brvggemann D, et al. Domain decomposition for an implicit LU-SGS scheme using overlapping grids[C]//13th Computational Fluid Dynamics Conference, 1997: 1896 [Google Scholar]
  16. Heffernan R M, Gaubert M. Structural and aerodynamic loads and performance measurements of an SA349/2 helicopter with an advanced geometry rotor[R]. NASA TM-88370, 1986: 1–58 [Google Scholar]
  17. Pomin H, Wagner S. Navier-Stokes analysis of helicopter rotor aerodynamics in hover and forward flight[J]. Journal of Aircraft, 2002, 39 (5): 813– 821 [Article] [CrossRef] [Google Scholar]
  18. Chandrasekhara M S, Martin P B, Tung C. Compressible dynamic stall control using a variable droop leading edge airfoil[J]. Journal of Aircraft, 2004, 41 (4): 862– 869 [Article] [CrossRef] [Google Scholar]

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