Numerical investigation of dynamic stall control using variable droop leading edge airfoil

被引:0
|
作者
Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China [1 ]
机构
来源
Hangkong Dongli Xuebao | 2008年 / 3卷 / 496-504期
关键词
Airfoils;
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 50 条
  • [21] Numerical investigation of air jets for dynamic stall control on the OA209 airfoil
    A. D. Gardner
    K. Richter
    H. Rosemann
    CEAS Aeronautical Journal, 2011, 1 (1-4) : 69 - 82
  • [22] Numerical investigation of self-sustained oscillations of stall cells around a leading edge-separating airfoil
    Bouchard, M.
    Marty, J.
    Deck, S.
    Costes, M.
    PHYSICS OF FLUIDS, 2022, 34 (11)
  • [23] Active control of leading-edge dynamic stall
    Greenblatt D.
    International Journal of Flow Control, 2010, 2 (01) : 21 - 38
  • [24] Dynamic stall control by leading edge vortex generators
    Mai, Holger
    Dietz, Guido
    Geissler, Wolfgang
    Richter, Kai
    Bosbach, Johannes
    Richard, Hugues
    de Groot, Klaus
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2008, 53 (01) : 26 - 36
  • [25] Numerical Investigation of Jet Angle Effect on Airfoil Stall Control
    Kim, Junkyu
    Park, Young Min
    Lee, Junseong
    Kim, Taesoon
    Kim, Minwoo
    Lim, Jiseop
    Jee, Solkeun
    APPLIED SCIENCES-BASEL, 2019, 9 (15):
  • [26] Numerical study of airfoil dynamic stall
    Qian, Wei-Qi
    Fu, Song
    Cai, Jin-Shi
    Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 2001, 19 (04):
  • [27] Investigation of dynamic stall through the application of leading edge roughness
    Green, R.B.
    Aeronautical Journal, 1994, 98 (971):
  • [28] Numerical Investigation of Leading Edge Blowing and Optimization of the Slot Geometry for a Circulation Control Airfoil
    Jensch, C.
    Pfingsten, K. C.
    Radespiel, R.
    NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS VII, 2010, 112 : 183 - 190
  • [29] Dynamic Stall Control Using Deployable Leading-Edge Vortex Generators
    Le Pape, A.
    Costes, M.
    Richez, F.
    Joubert, G.
    David, F.
    Deluc, J. -M.
    AIAA JOURNAL, 2012, 50 (10) : 2135 - 2145
  • [30] Numerical Investigation of Pulsed Air Jets for Dynamic Stall Control on the OA209 Airfoil
    Gardner, A. D.
    Knopp, T.
    Richter, K.
    Rosemann, H.
    NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS VIII, 2013, 121 : 287 - 295